JPH0766100B2 - Automatic focus adjustment device - Google Patents

Description

BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an automatic focusing device for a camera.

2. Description of the Related Art Conventionally, a defocus (hereinafter abbreviated as DF) amount and direction of a taking lens is detected, a driving amount for driving the taking lens is calculated based on the DF amount, and the calculated driving amount and An automatic focus adjustment device has been proposed that drives a taking lens to a focus position based on the DF direction.

In such an automatic focus adjustment device, since an approximate expression is used when calculating the drive amount from the DF amount, the calculated drive amount includes some error. Therefore, the in-focus state may not be obtained even after the above driving is completed.

Therefore, in order to solve this problem, in Japanese Laid-Open Patent Publication No. 59-204810, focus detection is performed again after driving for the calculated driving amount is completed, and it is confirmed whether or not a focused state is really obtained. An automatic focusing device configured as described above has been proposed.

Problems to be Solved by the Invention According to the device proposed in the above publication, the in-focus state can be surely obtained. However, there is a problem that it is not possible to immediately respond to a photo opportunity.

Therefore, an object of the present invention is to provide an automatic focus adjustment device in which the device disclosed in the above publication is further improved to shorten the time required for automatic focus adjustment without impairing the focusing accuracy.

Means for Solving the Problems In order to solve the above-mentioned object, the present invention provides a focus detection means for calculating a defocus amount of a photographing lens, a driving means for driving the photographing lens, and a driving means based on the defocus amount. Drive amount calculation means capable of calculating the drive amount of, and when the defocus amount exceeds a predetermined focusing width, the drive means is driven based on the calculated drive amount to focus the photographing lens. When the defocus amount does not exceed the predetermined focusing width, the drive means is stopped to drive the photographing lens, and the drive control means does not drive the photographing lens. After the driving is completed, the focus detection means is operated again, and based on the obtained detection result, the focus confirmation means for confirming whether or not the focus is achieved, and whether or not the defocus amount is equal to or less than the predetermined deviation amount are determined. When it is determined that the defocus amount is not less than or equal to a predetermined shift amount, the first focusing determination is performed by the focusing checking unit after the driving control unit finishes driving the driving unit. Means and the defocus amount is determined to be less than or equal to a predetermined deviation amount, it is determined to be in focus without performing confirmation by the focus confirmation means after the drive control unit has finished driving the drive unit. It is characterized by having two focus determination means.

In other words, paying attention to the fact that when the DF amount is small, the error contained in the calculated drive amount is small, and sufficient focusing accuracy can be obtained when the driving is completed. It is characterized by shortening the time until the end of focus adjustment by configuring, and when the DF amount is large, the error included in the calculated drive amount is large, so the focus is confirmed to maintain high focus accuracy. It is a thing.

According to the present invention, when it is determined that the DF amount is not less than or equal to the predetermined value, it is determined to be in focus when the focus is confirmed by the focus confirmation means, and the defocus amount is less than or equal to the predetermined value. When it is determined that the in-focus state is determined to be in-focus when the drive control unit finishes driving the drive unit without operating the focus confirmation unit.

Embodiment An outline of a camera system for automatic focusing according to an embodiment of the present invention will be described with reference to FIG. In FIG. 1, the left side of the alternate long and short dash line is the zoom lens (LZ), the right side is the camera body (BD), and both of them are the clutch (106).
Connection terminals (JL1) to (JL5) mechanically via (107)
(JB1) to (JB5) are electrically connected. In this camera system, the subject light that has passed through the focusing lens (FL) of the zoom lens (LZ), the zoom lens (ZL), and the master lens (ML) is at the center of the reflection mirror (108) of the camera body (BD). The optical system is configured so that the light is transmitted through the semi-transmissive portion of, and is reflected by the sub mirror (109) and received by the CCD image sensor (FLM).

The interface circuit (112) is a focus detection module (A
Driving the CCD image sensor (FLM) in the FM)
It captures subject data from the image sensor (FLM) and sends this data to the AF controller (113). The AF controller (113) calculates the defocus amount | ΔL | indicating the amount of deviation from the in-focus position and the defocus direction (front focus, rear focus) based on the signal from the CCD image sensor (FLM). To do. The motor (MO1) is driven based on these signals, and its rotation is transmitted to the zoom lens (LZ) via the slip mechanism (SLP), the drive mechanism (LDR), and the camera body side clutch (107).
The slip mechanism (SLP) prevents the motor (MO1) from being overloaded by slipping when the driven part of the zoom lens (LZ) receives a torque of a predetermined value or more.

In the zoom lens (LZ), the focusing lens (F
A female helicoid screw is formed on the inner circumference of the focus adjusting member (102) for driving L), and a fixing portion (101) integrated with the lens mount (121) is fitted to the female helicoid screw. ) Is formed with a male helicoid screw.
A large gear (103) is provided on the outer periphery of the focus adjusting member (102), and the large gear (103) is attached to the lens side clutch (106) via the small gear (104) and the transmission mechanism (105). It is connected. As a result, the rotation of the motor (MO1) is controlled by the slip mechanism (SLP) of the camera body and the clutch (10
7), through the clutch (106) on the lens side, the transmission mechanism (105) inside the lens, the small gear (104) and the large gear (103),
The focus lens (FL) is transmitted to the focus adjusting member (102) and moved back and forth in the optical axis direction by the helicoid screw to adjust the focus. An encoder (ENC) for monitoring the drive amount of the lens (FL) is connected to the drive mechanism (LDR) of the camera body (BD), and the encoder (ENC) changes the drive amount of the lens (FL). A corresponding number of pulses are output.

Here, the number of rotations of the motor (MO1) is NM (rot), the number of pulses from the encoder (ENC) is N, the resolution of the encoder (ENC) is ρ (1 / rot), and the rotation axis of the motor (MO1) is the encoder. Reduce the reduction ratio of the mechanical transmission system up to the (ENC) mounting shaft to μ
P, the reduction ratio of the mechanical transmission system from the rotary shaft of the motor (MO1) to the camera body side clutch (107) is μB, and the reduction ratio of the mechanical transmission system from the lens side clutch (106) to the large gear (103) is μL. , LH (mm / rot) for the helicoid lead of the focus adjustment member (102) and Δd (mm) for the movement amount of the focusing lens (FL), N = ρ · μP · NM Δd = NM · μB · μL · LH That is, the relational expression of Δd = N · μB · μL·LH / (P · μP) (1) is obtained.

Further, when the ratio of the movement amount ΔL (mm) of the image plane when the lens is moved by Δd (mm) and the above Δd is represented by Kop = Δd / ΔL (2), it can be expressed by equation (1) ( From 2) N = Kop ・ ΔL ・ ρ ・ μP / (μB ・ μL ・ LH) ……
The relational expression of (3) is obtained. Here, if KL = Kop / (μL·LH) (4) KB = ρ · μP / μB (5), then the relational expression of N = KB · KL · ΔL (6) is obtained. .

In the equation (6), ΔL is obtained from the signal processing circuit (112) as a defocus amount | ΔL | and a signal in the defocus direction. The KL in equation (4) is a zoom lens (L
It is output from the lens circuit (LEC) corresponding to the focal length set by the rotating operation of the zoom ring (ZR) for zooming operation (Z). That is, the code plate (FCD) outputs data corresponding to the rotational position of the zoom ring (ZR), this data is sent to the lens circuit (LEC), and the address corresponding to the data from this code plate (FCD) The KL data stored in is read serially by the reading circuit (LDC) of the camera body. The code pattern of the code plate (FCD) is determined so as to output data corresponding to the zoom ring (ZR) and the rotation setting position. Also, in the fixed storage means such as ROM built in the lens circuit (LEC), the KL data corresponding to the focal length set by the zoom ring (ZR) is the data from the code plate (FCD). Is fixedly stored in advance at an address corresponding to.

Further, KB in the equation (5) is data fixedly determined according to the reduction ratio μB in the camera body, and this data KB
Is owned by the camera controller (111).

Here, from the camera main body side reading circuit (LDC) to the lens side lens circuit (LEC), power is supplied via terminals (JB1) (JL1) and synchronization clock is supplied via terminals (JB2) (JL2). A read start signal is sent to each pulse via terminals (JB3) (JL2). In addition, data K is transferred from the lens circuit (LEC) to the reading circuit (LDC) via terminals (JL4) (JB4).
L is output in series. The terminals (JB5) (JL5) are common ground terminals.

When a read start signal is input via the terminals (JB3) (JL3), the lens circuit (LEC) sends KL data corresponding to the focal length set by the zoom ring rotation setting from the camera body to the terminals (JB2) (JL2). ), And outputs to the reading circuit (LDC) in series in synchronization with the clock pulse input via. And
The reading circuit (LDC) reads serial data from the terminal and converts it into parallel data based on the same clock pulse as the clock pulse output to the terminal (JB2).

The camera controller (111) uses the data KL from the reading circuit (LDC) and the data KB inside it as KL · KB = K.
Is calculated. The AF controller (113) calculates the defocus amount | ΔL | using the data of the subject image from the interface circuit (112), and this defocus amount | ΔL |
And the data K from the camera controller (111), K · | ΔL | = N is calculated to calculate the number of pulses to be detected by the encoder (ENC). The AF controller (113) rotates the motor (MO1) clockwise or counterclockwise through a motor driver circuit (114) according to a defocus direction signal obtained using the subject image data, and an encoder (EN
When the number of pulses equal to the value N calculated by the AF controller (113) is input from C), the focusing lens (FL)
Is determined to have moved by the amount of movement Δd to the in-focus position,
Stop the rotation of the motor (MO1). In the above explanation,
The data KB was fixedly stored on the camera body (BD) side, and the value of K = KL · KB was calculated by multiplying this data KB by the data KL from the lens, but the K value was calculated using the above method. It is not limited. For example, if the zoom lens can be attached to any of multiple types of camera bodies with different KB values, the lens circuit (LEZ) of the zoom lens (LZ)
From C), output the data of K1 = KL · KB1 corresponding to the camera body having a specific KB value according to the set focal length.
On the other hand, in the camera body of this specific model, the data KB in the camera controller (111) and the data K1 from the reading circuit (LDC) are not necessary for the calculation of KL / KB and the AF controller (1
13) and has a value KB2 (≠ KB1) different from the KB value of the above characteristics, when the above lens is attached to another camera body, the KB2 / KB1 value in the camera controller (111) You may make it have data and perform the operation of K2 = K1 · KB2 / KB1 = KL · KB2 to obtain the value of KL · KB2.

In particular, in the case of a front lens group type zoom lens in which the focusing lens (FL) is arranged in front of the zoom lens (ZL) as described above, the value of Kop is Kop = (f1 / f) ² …… (7) f1: It becomes the focal length of the focusing lens, and the KL value or K value for one zoom lens changes in a very wide range. In this case, the data KL or K stored in the lens is the exponent part data and the significant digit data (for example, in the case of 8-bit data, the upper 4 bits are the exponent portion and the lower 4 bits are the significant digit number). By dividing the lower 4 bits of the data read by the reading circuit (LDC) of the camera body into the camera controller (111) by shifting the data of the exponent part, the value of KL or K can be greatly increased. Even if it changes to, it can fully respond.

In the description of FIG. 1 above, the device of the present invention is shown to be configured by a combination of circuit blocks in order to facilitate understanding of the overall function and operation of the present invention. Most of the functions of these circuit blocks are achieved by a microcomputer (hereinafter, referred to as a microcomputer), as described below.

FIG. 2 is a block diagram schematically showing a circuit in the camera of this embodiment.

In Fig. 2, (MNS) is a power switch, and (POR) is a power-on reset circuit that resets the AF microcomputer (MC1) and control microcomputer (MC2) described later according to the closing of the power switch (MNS). is there. (S1) is a switch that is closed by pressing the shutter release button one step (half-press), and the operation of photometry and automatic focus adjustment is started by this closing. (S2) is a switch that is closed when the shutter release button is pressed (pressed down) in two stages, and the exposure operation is started by this closing. (S4) is a switch that is closed when the winding of the film is completed.

(MC2) is the camera controller (111) shown in Fig. 1.
Is a microcomputer that controls the operation of the entire camera system in a sequence (hereinafter, referred to as a control microcomputer). A switch (S1) is connected to the terminal (I1), and switches (S2) (S4) are connected to the terminal (I2) via an AND circuit. (OSC) is an oscillator circuit for that operation. (MC1) functions as the AF controller (113) shown in FIG. 1, and is a microcomputer (hereinafter referred to as AF microcomputer) that controls the automatic focusing operation in sequence. The calculated focus adjustment state is displayed in the viewfinder by turning on one of the display LEDB (LEDL) (LEDM) (LEDR).

(SAF / M) is a switch for switching between automatic focus adjustment mode (hereinafter referred to as AF mode) and manual focus adjustment mode (hereinafter referred to as nonAF mode), which is AF when closed.
Mode, when it is open, it becomes nonAF mode, and its SAF
The / M signal is input to the terminal (PT6) of the control microcomputer (MC2). Here, the non-AF mode is provided with an FA mode in which the lens is not moved because the focus adjustment state is considered to be displayed, and a MANUAL mode in which the display is not performed. (SA / R)
Is the AF priority mode that performs shutter release after the completion of automatic focus adjustment and the switch (S2) even before the completion of automatic focus adjustment
When the shutter is closed, it is a switch that selectively switches between the shutter release priority mode in which the shutter is released according to the closing of the
AF priority mode, when released, it becomes release priority mode, and its SA / R signal is the control microcomputer (MC2) terminal (PT7)
Entered in. (MDR2) is a driver circuit for controlling the motor (MO2) for winding and rewinding the film, and the motor (MO2) is controlled by the MM and MN signals from the control microcomputer (MC2).
It controls the direction and amount of rotation in 2). MM, MN
Table 1 shows the relationship between the signals and the operation of the motor (MO2).

(EDO) transmits the manually selected mode among the exposure control modes such as program mode / shutter speed priority mode / aperture priority mode / manual mode to the control microcomputer (MC2) and is required for the exposure control in that mode. An exposure control setting circuit for transmitting information such as shutter speed, aperture value, film sensitivity, and exposure correction value to the control microcomputer (MC2). (BS1) and (BS2) are the data lines.

(LMC) is a photometric circuit, the ANI signal of which indicates a reference voltage for A / D conversion, the VRI signal of which indicates an analog photometric signal. These are respectively terminals (PT7) (PT7)
8) has been entered. (EXD) is the control microcomputer (MC2)
An exposure display circuit that displays the proper exposure value (shutter speed, aperture value, etc.) calculated in (BS3) is its data line. (EXC) is an exposure control circuit that controls exposure according to the proper exposure value (shutter speed, aperture value, etc.) calculated in the control microcomputer (MC2) and the set exposure value, and (BS4) is the data It is a line.

(FLS) indicates a circuit (hereinafter referred to as a flash circuit) in the electronic flash device attached to the camera.
S) is the terminal (ST
1) Connected to the camera side circuit by (ST2) (ST3) (ST4) (ST5) and (GND). This flash circuit (FL
The details of S) are shown in FIG.

FIG. 3 shows a flash circuit (FLS), in which (20) is a main switch, (22) is a power battery, and when the main switch (20) is closed, the voltage of the power battery (22) is changed. Is boosted by the DC-DC converter (24) and supplied to the main capacitor (28) through the diode (26).
(GND) is the ground terminal. The charge voltage of the main capacitor (28) is monitored by the charge monitor circuit (30), and when the voltage reaches a predetermined amount, the charge completion detection circuit (3
2) outputs the charge completion signal, which is the AND circuit (3
It is transmitted to the terminal (ST2) via 4). On the camera side,
After receiving this charge completion signal, a light emission start signal is output via the terminal (ST1), which causes the trigger circuit (3
6) is triggered, the SCR (38) becomes conductive and the flash discharge tube (4
0) starts to emit light by the energy of the main capacitor (28). This light emission start signal is also input to the light emission start monitor circuit (42), and this light emission start monitor circuit (42)
When the light emission start signal is received, the AND circuit (34) is closed to prevent transmission of the charge completion signal to the terminal (ST2). When the side light circuit (LMC) on the camera detects that proper exposure has been reached, the camera outputs a light emission stop signal to the terminal (ST3), and the light emission stop circuit (44) receives this light emission stop signal. Then, the light emission of the flash discharge tube (40) is stopped.

(45) is an AF that is closed to provide auxiliary illumination from the electronic flash device to detect the focus adjustment state when the subject is dark.
When the auxiliary light switch is closed, the terminal (ST5) outputs an AF auxiliary light OK signal indicating that illumination for focus detection by auxiliary light is possible. If the camera determines that this auxiliary light is required, the terminal (ST4)
An AF auxiliary light emission signal is input to the transistor, the transistor (46) becomes conductive, and the auxiliary light LED (48) emits light.

Returning to FIG. 2, (Sx) is the synchro switch of the camera,
(FLB) is a light emission control circuit that controls the light emission time of the electronic flash device. (LEC) and (LDC) are the lens circuit inside the lens and the reading circuit inside the camera, respectively, as in Fig. 1. When the lens is attached to the camera, both circuits are
1) to (JB5) and (JL1) to (JL5) are connected to each other. In the figure, (VL) is the power supply, (RES) is the read start signal, (CL) is the clock pulse, (DATA) is the data,
(G) indicates ground respectively. A clock pulse is input to the reading circuit (LDC) from the control microcomputer (MC2) terminal (SCK), and the reading circuit (LDC) is output from the control microcomputer (MC2) terminal (TXD) serial data output. Lens data is serially input to that terminal (RXD) according to the signal.

(FLM) is the CCD image sensor shown in FIG. 1, (IF1) is the sensor driving interface circuit, and (MDR1) is the first
A driver circuit (ENC) corresponding to (114) in the figure, which controls the driving of the lens driving motor (MO1), is an encoder similar to that in FIG.

4 and 5 are flowcharts showing the operation of the control microcomputer (MC2) shown in FIG. The operation of the system shown in FIG. 2 will be described below with reference to this flowchart. Before that, the names and contents of the flags used in this embodiment are shown in Tables 2 and 3.

In FIG. 4, when the switch (S1) is closed and an interrupt signal is input to the terminal (I1), the control microcomputer (MC2) starts its operation. First, in step S1, the release flag
Clear RLF. This flag is used to distinguish between continuous shooting (hereinafter referred to as transfer mode) and single-shot shooting (hereinafter referred to as single-shot mode) in the shooting modes of the camera. Here, the continuous shooting mode means the switch (S2)
When it is ON, it refers to the mode in which you can take pictures continuously, and single-shot mode refers to the mode in which one shot can be taken with one switch (S2) turned ON. Next, in S2, the AF microcomputer drive clock CK is supplied from the control microcomputer (MC2) terminal (Xout) to the AF microcomputer (MC1). Next, in S3, serial input / output operations are performed multiple times to capture multiple data from the lens circuit (LEC), and the conversion coefficient (KROM) necessary for automatic focus adjustment, the light of the wavelength emitted by the auxiliary light, and the visible light AF for determining whether focus detection calculation is possible for AF focus position correction data (△ IR), backlash data (BKLSH), AF (automatic focus adjustment) or FA (focus adjustment status display) For open F value (AFAV0), lens attachment discrimination (LENSF), presence or absence of AF coupler axis (AFCF), whether the lens can detect focus (FA
Save each signal of (ENL) in the memory in the control microcomputer (MC2). In step S4, data from the exposure control value setting circuit (EDO) that outputs setting data for exposure control and the like is fetched. This includes data relating to exposure and whether to use single-shot or continuous-shot mode. In S5, set the AFS signal output from the control microcomputer (MC2) terminal (P51) to "Low".
To This is the interrupt pin (INT of the AF microcomputer (MC1)
The signal is input to 1) and the AF
The microcomputer (MC1) starts operation. Terminal (PT2) at the same time
The INREL signal from is set to "High". This is input to the interrupt terminal (INT2) of the AF microcomputer (MC1), but this interrupt does not occur because the interrupt occurs at the falling edge.

In the flowchart of FIG. 4, there may be a case where a loop is made from S5 to S10 and S22 to S3. When passing S5 in the loop, the AFS signal falls and the INREL signal rises many times, but the AFS signal is already "Low" and the INREL signal is "High".
Therefore, the AF microcomputer (MC1) is not interrupted. When the operation of the AF microcomputer (MC1) is started, the setting data for the operation of the AF microcomputer (MC1) and the data from the lens are serially sent from the control microcomputer (MC2). The control microcomputer (MC2) terminal (TXD) is synchronized with the clock signal from the control microcomputer (MC2) terminal (SCK).
Serially outputs 5 bytes of 8-bit data and the contents shown in Table 4 are output, and the AF microcomputer (MC1) terminal (TXD)
Entered in.

The control microcomputer (MC2) is connected to the AF microcomputer (MC1) terminal (P1
DTRQ from 1) to control microcomputer (MC2) terminal (PT4)
The signal is regarded as a signal of data request, and data output is started. In the control microcomputer (MC2), this DTRQ signal is "Lo" in S6.
Wait until it becomes "w", and if it becomes "Low", proceed to S7 and send the data. The AESIO of S7 makes the data to determine the operation mode of the AF microcomputer (MC1) and sends the data serially. However, it is shown as another routine in FIG.

At the beginning of the AESIO routine starting from step S29 in FIG. 5, first, the RAM of the fifth serial data of the control microcomputer (MC2) containing the signals AFFL, RDY, DR, AFC, FAEN is cleared. The FAEN signal is determined in S30, S31, and S32. First S30
Check the LENSF signal of the data coming from the lens circuit (LEC), and if LENSF = 0 indicates no lens, the FAEN signal remains “0” and the process proceeds to S33. If the lens is attached and LENSF = 1, if the FAENL signal is "1", that is, if the lens is focus-detectable, go to S32 and set the FAEN signal to "1". is 0"
Will remain.

Next, in S33 to S35, the AFC signal is determined. Terminal at S33 (PT
Check the SAF / M signal input to 6). The SAF / M signal is a switch that decides whether or not to automatically adjust the focus of the camera lens from outside the camera. If it is "High", the AF mode (the focus adjustment state of the shooting lens mounted in the camera body is detected, Depending on the result, the mode for automatically adjusting the focus of the taking lens), and if it is "Low", it will be the non-AF mode. S33
If the SAF / M signal is “0” in, the AFC signal remains “0” in S36.
If it is "1", go to S34 and use the data A from the lens.
Watch the FCF signal. If the AFCF signal is "1" in S34, select the lens
Since there is a coupler axis for AF, set the AFC signal to "1" in S35. That is, when the lens has the coupler axis for AF and the operation switch (SAF / M) of the camera is closed to be on the AF side, the AFC signal becomes "1", and other than that, it is set to "0".

If the camera drive mode setting in S36 and S37 is continuous shooting mode, the DR signal is set to "1", and in single shooting mode, the DR signal remains "0". Next, in S38 and S39, the signal from the electronic flash device attached to the camera is checked, and if the electronic flash device is attached to the camera and the AF auxiliary light switch (45) is on, the flash circuit (FLS) The terminal (ST5) goes into the "High" state and enters the terminal (PT11). At S38, PT11 =
If it is "High", the AFFL signal is set to "1" in S39. This is a signal to the AF microcomputer (MC1) that the AF auxiliary light can be emitted. (Details will be described later.) Set the RDY signal in S40 and S41. When charging of the electronic flash device is completed, the terminal (ST2) of the flash circuit (FLS) goes to the "High" state, and this is input to the terminal (PT9). Go ahead and set the RDY signal to "1". This signal is also used at the time of focus detection using auxiliary light described below (hereinafter referred to as auxiliary light AF mode). Then, AF the data sent from the lens in S42
Set it in the serial transfer register to send it to the microcomputer (MC1). In S43, C to start serial transfer
Set the SAF signal to "High". This is an AF microcomputer (MC1)
In response to the DTRQ signal of the serial transfer request from CS
When the AF signal becomes "High", the AF microcomputer (MC1) starts capturing serial data. Then, in S44, the 8-bit 5-byte data is transferred to the AF microcomputer (MC1). S45
Then, the CSAF signal is returned to "Low" and the serial transfer is completed.

Next, return to the main routine of FIG. 4 and perform the next step.
Go to S8. Here, from the photometry circuit (LMC),
Taking in the NI signal and the VRI signal of the reference voltage for A / D conversion,
A / D convert the photometric output and prepare it as the data required for exposure calculation. Next, in S9, the exposure calculation for the constant light and the flash light is performed. At the next step S10, it is checked whether the terminal (I2) of the control microcomputer (MC2) is "Low" to see if the release has been made. If the shutter is charged, the switch (S4) is on, the release button is pressed in two steps, and the switch (S2) is turned on, the terminal (I2) should be "Low". Terminal (I2) is "High"
If so, proceed to S25 because it has not been released. In S25, the release flag RLF is cleared. Then, in step S26, it is determined whether or not the charging completion signal is received from the electronic flash device, and if the charging completion signal is received, S2
Proceed to 7 to send the flash light photographing data to the display unit (EXD), and if the charging completion signal is not received, proceed to S28 to send the constant light photographing data to the display unit (EXD) for display and display the data in step S22.
Move to. Then, in step S22, it is determined whether the terminal (I1) is "Low" with the switch (S1) still closed, and if it is "Low", the process returns to step S3 and the same operation as described above is performed. repeat.

On the other hand, when it is determined in step S22 that the terminal (I1) is "High", the process proceeds to S23, and the operation of the AF microcomputer (MC1) is stopped. The way to stop is to interrupt the AF microcomputer (MC1) terminal (INT1) with the AFS signal. Start of AF microcomputer (MC1) by AFS signal and AF
In order to distinguish it from the interruption for stopping by the S signal, the stop interrupt is made to rise again in less than 50 μs after falling (see FIG. 17 (B)). If only the metering flow is interrupted from S26 to S28,
Since the AFS signal is “Low”, the stop signal is once “Hig
Release after "h", flow of release S11 ~ S21
When an interrupt occurs, the AFS signal is "High", so the stop signal falls. This interrupt causes the AF microcomputer (MC1) to enter stop mode and stop the automatic focus adjustment operation. In S24, the exposure display on the display (EXD) is turned off, and the control microcomputer (MC2) stops operating.

Next, if photometry is repeated and the flow is released in the middle of looping, the terminal (12) becomes "Low". Then S1
Check 0 and go to S11. Next, release flag RL
Check F and if 1, go to S26. This means that if the shutter is released once in single shooting mode, the release flag RLF is set to 1 in S21 to S22, and if the switch (S2) is turned on by pressing the release button two steps,
Not released again. On the other hand, if the switch (S2) is turned off while the switch (S1) is turned on, step S10
From S25, the release flag RLF is cleared. That is, when the switch (S2) is turned on again next time,
It will be released from S11 to S12.

Next, in S12, the AF priority / release priority switching signal input to the terminal (PT7) is checked. Here, the AF priority mode is a mode in which the shutter is released only after focusing is completed by the automatic focus adjustment even if the switch (S2) is turned on.The release priority mode is the focus during automatic focus adjustment. Is a mode that releases any time the switch (S2) is closed. In S12, SA / R signal is "Hig
If h "(SA / R = 1), the AF priority mode is set, and the process advances to S13 to check the AFE signal. This is the AF microcomputer (MC
When the AF microcomputer (MC2) detects the focus by the signal output from the terminal (P12) of 1) and determines that it is in focus, “Hig
It is a signal which becomes "h". In S13, it is determined whether or not it is in focus. If it is in focus, the AFE signal is "1" and the flow advances to S14 to enter the release. If the signal is “0”, it goes to S26 and is not released. On the other hand, if the release priority mode is at S12, it goes to S14 and is released. The SA / R signal to be checked at S12 is manually selected by the switch attached to the camera. Is a signal according to
This is also linked to a self-timer switch (not shown), and when the self-timer is activated, it switches to the release priority mode even if the switch is in the AF priority mode. During the self-timer, the release priority mode is set. When using the self-timer, S14 and S
Wait time for self-timer (not shown) between 15,
Wait for 10 seconds. Also, the switch (SA / R) provided on the camera body is connected to the terminal (PT7), but this switch is taken out of the camera body and used for an external controller (for example, a controllable back cover) or a remote controller. You can leave it to the receiver.

Next, in S14, an INREL signal indicating that the release has been made from the terminal (PT2) to the AF microcomputer (MC1) is issued. The INREL signal is input to the interrupt terminal (INT2) of the AF microcomputer (MC1), and the falling edge of this signal causes an interrupt, causing the AF microcomputer (MC1) to jump to the release routine. Then, even if the lens is being driven during automatic focusing, the operation is stopped, the display is turned off, and the release is completed. At S14, the AFS signal is set to "High" in preparation for the end of the next release and the start of the operation of the AF microcomputer (MC1). Next, in step S15, it is determined whether the charging completion signal is being input from the flash circuit (FLS) by looking at the terminal (PT9). Send to the exposure control circuit (EXC), and if the charging completion signal is not input, S17
Sends the exposure control data for continuous light to the exposure control circuit (EXC). Then, the exposure control operation is started in S18.

When the exposure control operation is completed, the film is automatically wound up in S19. Then, the release flag RLF described above in S20 and S21 is set to "1" in the single shooting mode, and the process proceeds to S22.
If the switch (S1) is still closed and the terminal (I1) of the control microcomputer (MC2) is "Low", step S3
After that, the control microcomputer (MC2) operates after the data acquisition, data calculation and display operations are repeated, and if the switch (S1) is not closed, the operation proceeds to step S23 and the same operation as described above is performed. To stop. This concludes the description of the flow of the control microcomputer (MC2).

FIG. 6 is a circuit diagram showing details of the interface circuit (IF1) of this embodiment. The operation of this circuit will be described below.

When the control microcomputer (MC2) detects that the switch (S1) that is closed by pressing the shutter release button one step is ON, the AF microcomputer (MC1) performs focus adjustment operation according to the signal from the control microcomputer (MC2). To start.

First, the IOS signal from the AF microcomputer (MC1) is set to "Low", and the interface circuit (IF
The gate opens in the direction in which the signals of NBφ to NB3 are output toward 1). Then, the AF microcomputer (MC1) outputs a pulsed integration clear signal ICG to the CCD image sensor (FLM) as a signal of NB2, which causes the CCD image sensor (F
Each pixel of LM) is reset to the initial state and CCD
The output AGCOS of the brightness monitor circuit (MC) built in the image sensor is reset to the power supply voltage level. AF
At the same time, the microcomputer (MC1) receives a "Hig" from the terminal (NB5).
The shift pulse generation enable signal SHEN of h "level is output.
Then, at the same time as the integration clear signal ICG disappears, the integration of photocurrent starts in each pixel in the CCD image sensor (FLM), and at the same time, the output AGCOS of the brightness monitor circuit (MC) drops at a speed according to the brightness of the subject. To start, the reference signal output DOS from the reference signal generation circuit (RS) built into the CCD image sensor is kept at a constant reference level. The AGC controller (406) compares AGCOS with DOS, and controls the gain of the variable gain differential amplifier (408) according to how much AGCOS decreases with respect to DOS within a predetermined time (100 msec. During focus detection). To do. Further, when the AGC controller (406) detects that AGCOSB has decreased to a predetermined level or more with respect to DOS within a predetermined time after the integration clear signal ICG disappears, at that time, it outputs a "High" level TINT signal. This TINT signal is input to the shift pulse signal output circuit (410) through the AND circuit (AN) and the OR circuit (OR1), and in response thereto, the shift pulse SH is output from this circuit (410).
Also, the TINT signal passes as an NB4 signal through the OR circuit (OR2).
The signal is taken into the AF microcomputer (MC1) and the AF microcomputer (MC1) knows the completion of integration of the CCD image sensor by this signal. When this shift pulse SH is input to the CCD image sensor (FLM), the photocurrent integration by each pixel ends, and the charge according to this integration value is transferred in parallel to the corresponding cell of the CCD image sensor shift register. . On the other hand, based on the clock pulse CL from the AF microcomputer (MC1), the sensor drive pulse generation circuit (412) outputs two sensor drive pulses φ1 and φ2 with a phase difference of 180 °, and the CCD
Input to the image sensor (FLM). CCD image sensor (FLM) has φ
In synchronization with the rising edge of 1, the charge of each pixel of the CCD shift register is discharged serially from the end one by one, and the OS signal forming the image signal is sequentially output. This OS signal has a higher voltage as the intensity of incident light to the corresponding pixel is lower, and the subtraction circuit (414) subtracts this voltage from the reference signal DOS described above,
(DOS-OS) is output as a pixel signal. If the TINT signal is not output after the integration clear signal ICG disappears and a predetermined time elapses, the AF microcomputer (MC1) outputs "H" from the terminal (NBφ).
The igh "level shift pulse generation command signal SHM is output. Therefore, if the" High "level TINT signal is not output from the AGC controller (406) even after a lapse of a predetermined time after the integration clear signal ICG disappears, this shift In response to the pulse generation command signal SHM, the shift pulse generation circuit (41
0) generates the shift pulse SH.

On the other hand, in the above-described operation, the AF microcomputer (MC1) outputs the sample hold signal S / H when the pixel signals corresponding to the 7th to 10th pixels of the CCD image sensor are output. This part of the CCD image sensor is covered with an aluminum mask for the purpose of removing the dark output component, and the light receiving pixel of the CCD image sensor is in a light-shielded state. on the other hand. The peak hold circuit (416) holds the difference between the output OS and DOS corresponding to the aluminum mask part of the CCD image sensor by the sample hold signal, and this difference output and the pixel signal are input to the variable gain amplifier (408) thereafter. To be done. The variable gain amplifier (408) amplifies the difference between the pixel signal and its difference output with a gain controlled by the AGC controller (406), and the amplified output is A / D converted by the A / D converter (418). After that, it is taken into the AF microcomputer (MC1) as pixel signal data.

When the pixel signal data is captured, the AF microcomputer (MC
Signal IOS from 1) becomes "High", and NBφ to NB from the interface circuit (IF1) to the AF microcomputer (MC1)
The gate opens in the direction where the 3 signal is output. The A / D conversion of the A / D conversion circuit (418) is performed by 8 bits, but the upper 4 bits and the lower 4 bits are transferred to the AF microcomputer (MC1).
The switching timing of the upper and lower 4 bits is EOC
It is done by signals. The EOC signal is ORed with the TINT signal by the OR circuit (OR2) and input to the AF microcomputer (MC1) as the NB4 signal. AF microcomputer (MC1) is this NB
Depending on the timing of the “High” and “Low” states of the four signals
Pixel signal data will be fetched from NBφ to NB3.
Further, AGC data is also fetched from the NBφ to NB3 from the AGC controller (406) before the fetching of pixel signal data is started. This AGC data is
As will be described later, it is used as a judgment level. In addition, the Sφ signal output from the terminal (NB1) of the AF microcomputer (MC1) is used to initialize the CCD image sensor.
This is a signal for switching between normal operation for integrating the subject light.

After that, the AF microcomputer (MC1) sequentially stores this pixel signal data in the internal memory. When the data corresponding to all the pixels of the image sensor has been saved, it is used to defocus according to a predetermined program. And the direction thereof are calculated and displayed on the display circuit. On the other hand, the lens driving device is driven according to the amount of defocus and the direction of the defocus to automatically adjust the focus of the taking lens.

In the present embodiment, the integration of the CCD image sensor (FLM), the data dump, and the focus detection calculation are repeated to improve the accuracy.

7 to 16 are flowcharts showing the operation of the AF microcomputer (MC1). First, Tables 5-1, 2, and 3 show the flags used in this flowchart.

There are four entrances to start the operation of the AF microcomputer (MC1). In other words, when the power is turned on, that is, when the RES signal arrives at the terminal (CLR1) of the AF microcomputer (MC1) in FIG. 2, “RESET” (step # 1 in FIG. 7), the terminal of the control microcomputer (MC2) ( Issue to start AF operation (automatic focus adjustment operation) or FA operation (focus detection operation) from PT1)
"INTIS" (step # 8 in Fig. 7) started when the AFS signal is input to the pin (INT1) of the AF microcomputer (MC1), the pin (PT2) of the control microcomputer (MC2) to the AF microcomputer (MC1) I give it out to let you know that I have released
"INT2S" (step # 27 in Fig. 8) started when the NREL signal is input to the terminal (INT2) of the AF microcomputer (MC1), and the PS signal from the encoder (ENC) is the terminal of the AF microcomputer (MC1) “INT3S” (step # 252 in FIG. 16) started by being input to (INT3) corresponds to these four. The main routine of the flow of the automatic focus adjustment operation starts from "INT1S" in step # 8 in FIG. 7 and goes through "AFSTART" in step # 33 in FIG. 9 and "CDINTS" in step # 44 in FIG. 11 Flow to “MAIN1” in step # 86 in FIG. From "MAIN1", it is roughly divided into three. From the flow of low contrast where the contrast of the subject is low starting from "LOWCON" in step # 165 in Fig. 13 and "LSAVE" in step # 238 in Fig. 14 Auxiliary light AF mode that starts (it is a mode that illuminates the subject with the auxiliary light LED (48) to detect the focus when it is dark and focus detection is not possible), and step # 91 in FIG. The flow is for normal AF mode, in which the contrast of the subject begins with "NLOC1" and is sufficiently high. As a subroutine, the flow of inputting and processing serial data from the control microcomputer (MC2) starting with "SIOSET" in step # 241 of Fig. 15 and the end of the lens starting from "CKLOCK" of step # 196 in Fig. 14 There is a flow for judging the position. The automatic focus adjustment operation (hereinafter referred to as AF operation) and the focus detection operation (hereinafter referred to as FA operation) in this embodiment will be described below based on this flowchart.

First, in response to the closing of the power switch (MNS), a reset signal RES is output from the power-on reset circuit (POR), and this control signal causes the control microcomputer (MC2) to move from a specific address. At the same time, the clock pulse CK is output from the terminal (Xout) of the control microcomputer (MC2). This is input to the terminal (Xin) of the AF microcomputer (MC1). When the reset signal RES is input to the terminal (CLR1) under the clock pulse CK from the control microcomputer (MC2), the AF microcomputer (MC1) starts from “RESET” in step # 1.
Step # 1 clears all the flags (Tables 5-1, 2, and 3) used in the flowchart. Each flag is set to "0" in the initial state. From step # 2, to stop AF or FA operation from the control microcomputer (MC2) to the AF microcomputer (MC1),
Although a stop signal as will be described later is output, this step # 2 is also passed when this stop command is input.

In step # 2 (hereinafter “step” is omitted), the signal from the terminal (ST4) input to the terminal (P13) is brought to the “Low” state and the illumination by the auxiliary light LED (48) is turned off. This is the switch (S1) while the auxiliary light is emitting in auxiliary light AF mode.
This is because the light emission is stopped when the focus detection operation is stopped by opening. In # 3, the focus adjustment state display or the defocus direction display in the AF or FA operation is turned off. Here, "High" is output to the terminals (P32) to (P30) and erased, but this is done by setting each terminal to the input mode. Even if the display is turned off by this method, the output state that was being displayed is stored in the output port register.
By putting this port in output mode, the contents stored in memory can be displayed again. We will use this later.

In # 4, the lens is stopped. The brake is not applied here. This is because, while the AF microcomputer (MC2) is not operating, the lens is not braked so that it can be moved relatively easily by hand, and power saving is considered. The control of the lens motor drive signals MC, MR, MF, and MB that are input from the AF microcomputer (MC2) to the driver circuit (MDR1) are as shown in Table 6 and the terminal (PO2).
By setting the signals MR, MF, and MB of ~ (PO0) to the "High" state, the electric brake is not applied and the motor (MO1) is de-energized and the lens stops.

In # 5, when a stop command is received from the control microcomputer (MC2) during the release operation or the fill AF mode, the release flag (No. 5-1
This is a step of clearing the release F) in the table and the auxiliary light mode flag (the auxiliary light mode F in Table 5-2). # 6
Is a control for deciding the interrupt state for starting the next flow. After the operation of the AF microcomputer (MC1) stops, INT1S of # 8 or INT of # 28
It allows starting from 2S. However, in actuality, when the shutter release button (not shown) for the camera is pressed one step, the switch (S1) in FIG. 2 is closed and the control microcomputer (MC2) interrupts INT1. Switch (S2) is closed and IN
Since the release interrupt is applied to T2, the start of the next flowchart starts with "INT1S" in # 8.
become. At # 7, the AF microcomputer (MC1) enters stop mode. Stop mode means that the AF microcomputer (MC1) enters the power saving mode and stops operating. At this time, the status of each terminal is only "Low" for P13 and "High" for others, the LED for auxiliary light illumination (48) is off, and the LED for display (LEDL) (LE
DM) (LEDR) is off, the lens is in the stop state, and the interface circuit (IF1) is also in the stop state. In this state, the next control microcomputer (MC2)
Waiting for start of interrupt from pin to INT1.

Next, # 8 which is the second entrance of the above-mentioned flowchart
Move on to the explanation of "INT1S". The interrupt start from this "INT1S" does not disable the interrupt during the entire flow of the AF microcomputer (MC1) and accepts the interrupt at any time. This entrance serves three interrupts. One is the start of the AF or FA operation, the second is the stop of the AF or FA operation, and the third is the operation of returning the focus adjustment state display immediately after the release and the operation in the continuous shooting mode. These 3
Let us describe two distinctions. The first and the second are distinguished by the input signal to the terminal (INT1). That is, as shown in Fig. 17 (A), AFS is used to start AF or FA operation.
Signal falls from "High" to "Low", "Low" is 50μs
It is necessary to continue above. To stop the AF or FA operation, the AFS signal changes from "High" to "Low" as shown in Fig. 17 (B).
After falling to, within 50μs from "Low" to "High"
Need to get up to. A flag is used to distinguish the third operation from the first normal AF or FA operation. When a release interrupt described later comes, the release flag (release F) is set in the flow during release, and it is distinguished by checking whether or not this flag is set at the start of the next "INT1S". These will be sequentially described from # 8. # 8, INT at the start
Disable interrupts other than 1 and INT2. The event counter interrupt of INT3 and the internal interrupt of the timer that determines the blinking period of the display LED, which is not shown in the flowchart, are prohibited. # 9 is about to clear the used flag, but AFSINR from # 15
Among them, the two flags used as the previous states, that is, the scan prohibition flag (scan prohibition F in Table 5-1) and the previous low control flag (previous low control F in Table 5-1) are not cleared. The switch (S1) does not clear the scan prohibition flag even in continuous shooting mode.
As long as you do not turn off, once the contrast of the subject is sufficient for focus detection and you have been able to calculate the defocus amount, or once you have performed low contrast scan, as in the single shooting mode, This flag is left to prevent low contrast scanning. In addition, the reason why the low contrast flag is not cleared last time is "AFSINR" which is the interrupt flow by the AFS signal after release starting from # 15. If the switch (S1) remains on after release, The focus detection calculation result display is not cleared in order to restore it. That is, during release, the LED defocus direction display is turned off once, and when the release operation is finished, it is displayed again.Therefore, it is necessary to determine whether the LED was blinking at low contrast. Leave the flag.

Wait for 50μs in the next # 10, and check if the interrupt entered in "INT1S" was an AF or FA stop interrupt.
I will go to see it. Here, the pin of the AF microcomputer (MC1) (INT
If the signal in 1) is as shown in Fig. 17 (A), A
Since the FS signal is "Low", proceed to # 12. If the signal is as shown in FIG. 17 (B), the AFS signal becomes "High" and proceed to the stop mode processing flow "STPMD" of # 2. The operation of the AF microcomputer (MC1) stops. In # 12, AFS after release
Interruption flow by signal Go to "AFSINR" or first AF
Distinguish whether it is due to an S signal interrupt. That is, if the release flag (release F) is on, # 15 “AF
SINR "and if the release flag (release F) is not on, proceed to the next Step # 13. In # 13, each terminal of the AF microcomputer (MC1) is initialized. That is, only the auxiliary light emitting terminal (P13) in the auxiliary light AF mode is set to "Low" and the other terminals are set to "High". However A
When the F microcomputer (MC1) has been in the stop mode so far and has come to this step at interrupt start, each pin remains in the same state, that is, only the pin (P13) is "Low" and the others It remains “High”.

Next, in # 14, the scan prohibition flag and the previous low control flag which were not cleared in # 9 are cleared again.
Then proceed to # 33 “AF START”. After that, the focus adjustment state is detected, the lens is driven according to the result,
The focus adjustment status is displayed. What is the focus adjustment status display?
Input signals LL and LR of LED (LEDL) (LEDM) (LEDR) are “H”
igh ", LM is to turn on the green LED when it is" Low ". If you see this display and close switch (S2), or (S1) and (S2) are closed, auto focus If the adjustment is done and the focusing operation is completed, the control microcomputer (MC
2) starts the release operation and at the same time AF microcomputer (MC1)
An interrupt signal INREL is output to notify that the shutter has been released. Since the AF microcomputer (MC1) receives this at the pin (INT2), it causes a release interrupt. This is the flow starting from "INT2S" in # 27 of FIG.

In # 27, interrupts other than INT1 and INT2 are first disabled. Next, at # 28, the signal from the terminal (ST4) is set to "Low" to turn off the auxiliary light illumination. This is a step that is necessary only in the release priority mode and not necessary in the AF priority mode.
This is because the focus adjustment is completed in the AF priority mode and the auxiliary light illumination is already off. # 29
Similarly, this is a step of stopping the lens motor (MO1) required only in the release priority mode. Here, the motor (MO1) is not braked. In the release priority mode, it is not always possible to release after the subject is in focus, and it is possible that the release may occur before that, so it was released while the lens was moving toward the in-focus position. At that time, rather than brake the motor (MO1) at that non-focus point to stop the lens and release,
This is because it is often better to take a good picture by stopping without braking, moving the lens by some inertia, and then releasing the lens near the in-focus position. In # 30, the focus adjustment status display or defocus direction display disappears. This is because the mirror is raised and the inside of the viewfinder is completely black during the release with the single-lens reflex camera. This is because it is meaningless to display only the display here, and it is not preferable that unnecessary light is output inside the camera during film exposure.

Next, at # 31, set the release flag (release F) to "1",
The release is left as a flag. The rest is # 32
Then, wait for INT1 or INT2 interrupt. When the release interrupt comes in succession, it starts again from "INT2S" of # 27. This occurs when the switch (S2) is repeatedly opened and closed while the switch (S1) in Fig. 2 is closed, and this is the case where the lens is fixed at the in-focus position without being driven.
It is the same as repeating the release in the locked state. After the switch (S2) is closed and released, the switch (S1) remains closed, and the control microcomputer (MC2)
As shown in the flowchart, the AFS signal enters the AF microcomputer (MC1) again and INT1 interrupt occurs. Then,
The flow from "INT1S" of # 8 advances to "AFSINR" of # 15 of FIG. 7 because the release flag (release F) is set to 1 this time. The steps from # 15 will be described later.

Next, when the switch (S2) is closed and released, and then both switches (S2) and (S1) are opened as shown in the flow chart of FIG. ) Stop AFS signal enters AF microcomputer (MC1) and INT1 interrupt occurs. After that, the AF microcomputer (MC1) enters the stop mode by the above-mentioned flow and waits for the next interrupt again.

Here, the flow of interrupt start by the AFS signal after release will be described. The entrance is "INT1S" in # 8 in Figure 7.
However, since the release flag RLF is 1 this time, branch at # 12 and proceed to "AFSINR" at # 15. Here, first, the release flag (release F) is reset because this flow has been passed. Next, in # 16, input serial data from the control microcomputer (MC2). The serial data is input here to check whether the operation mode of the AF microcomputer (MC1) has been changed. The flow that comes to "AFSINR" starting from # 15 is the flow that comes after the release.
Each mode of MANUAL mode, or single shooting mode in AF mode /
If the continuous shooting mode is changed), the operation must be changed according to the mode. # 16 is a step for inputting the information of this mode from the control microcomputer (MC2). This # 16 is a subroutine # 24 in Figure 15.
The flow of "SIOSET" starts from 1. Here, each mode is checked and the mode flag is operated. First, in # 241, head toward the control microcomputer (MC2) (P1
Set the DTRQ signal in 1) to "Low" to request serial data. Then, the control microcomputer (MC2) sees the DTRQ signal and the fourth
It sends serial data as shown in the table. On the AF microcomputer (MC1) side, input this serial data with # 242,
Set the DTRQ signal to "High" in # 243. Data sent by serial communication are AF open F value AFAV0, lens drive defocus amount-pulse count conversion coefficient KROM, auxiliary light AF correction data ΔIR, lens drive inversion backlash correction data BKLSH , Auxiliary light OK signal AFFL, flash charge completion signal RDY, continuous shooting / single shooting mode signal DR, AF
Lens signal AFC with coupler shaft, FA enable / disable signal FAEN 9
It is a seed. When each information is sent by serial communication
It is saved in the RAM of the AF microcomputer (MC1), and the contents of that RAM will be referred to when necessary. The use of each information will be described later in the explanation of the flowchart.

From # 244, check each mode. In step # 244, the AF open F value AFAV0 is checked. The light receiving element for focus detection has a usable limit, and if the open F value of the lens is small, the incident light on the light receiving element for focus detection is eclipsed by the exit pupil, and correct focus detection calculation cannot be performed. Even if a single lens that makes focus detection impossible is not created, the focus detection limit F value may be exceeded depending on the combination of converter lenses and the like. For example, if the focus detection limit F value of the focus detection light receiving element is 7.0, a lens with an open F value of 5.6 for AF can detect focus, but if a double teleconverter is attached to this, the F value will be 11.2 and focus detection will be impossible. It means that Here, the AF open F value is the F value when the diaphragm of the lens is not closed, but even in the case of a lens whose F value changes due to zooming or focusing, the focus detection light receiving element is not cut off. Since this is information for determining that, if the F value changes due to zooming or focusing, the smallest open F value is included. If the open F value AFAV0 for AF is larger than 7.0 in # 244, proceed to # 251, set the AF mode flag (AF.F in Table 5-1) to “1”, and then in # 250. F
Also set the A mode flag (FA.F in Table 5-1) to "1" and MANUA
Set the flag state that it is in the L mode, # 16 in FIG.
Go back. F for open F value AFAV0 for AF is less than 7.0
Regarding the value, it is a lens that can detect focus # 245
Go to.

In # 245, it is checked whether it was in AF mode so far. If the AF mode flag is "0"
If it is "1", it means that it was not in AF mode and it is checked whether it is FA mode or MANUAL mode. # 246 is a step to check whether there is an AF coupler axis. If the AFC signal is "1", there is an axis, so proceed in AF mode as it is, and if it is "0", there is no axis and automatic focus adjustment cannot be done. In # 247
Go to and set "1" to the AF mode flag. The AF coupler shaft is a shaft for transmitting power from the motor (MO1) in the camera body to the focusing mechanism of the lens.

In # 247 of FIG. 15, it is checked whether or not the lens can detect the focus. If the focus can be detected, the FA flag (FA.F) is set to "0" to enter the FA mode. If the focus cannot be detected, the FA flag is set to "1". Then, it is judged that the AF flag is "1" and the mode is MANUAL mode. When FAEN = 1, it means that the lens is attached to the camera body and the focus can be detected. Other than this, FAEN is “0”. A lens whose focus cannot be detected is a lens such as a reflective telephoto lens whose focus cannot be detected even if the open F value for AF is small, or a special lens such as a shift lens or a vari-soft lens in which aberration becomes extremely large. This subroutine does not see the change from FA mode to AF mode, but this will be seen later in step # 86 in FIG.

Now, the subroutine of FIG. 15 returns and proceeds to the next step # 17. Check if it is AF mode. If it is AF mode, go to # 19. If it is not AF mode, go to # 18.
Check in FA mode to see if it is not FA mode, and proceed to # 36 “MANUAL” flow.

In # 19, if the state before release is low contrast when looking at the previous state for display restoration, the low contrast display is restored in # 20. The low contrast display is a display in which both ends (LEDL) (LEDR) of the three LEDs (LEDL) (LEDM) (LEDR) for focus adjustment state display are blinked by repeatedly turning on and off at 2 Hz. If the contrast is not low, the focus adjustment state or the direction display is restored in # 21. The contents displayed before the release are saved in the display register, so the previous display is restored when the port is set to output mode. In # 22, by the AF mode flag (AF.F)
Check if it is in AF mode, FA not in AF mode
If it is the mode, go to # 39 “CDINTA” to repeatedly perform focus detection. Therefore, in the FA mode, if the switch (S1) in FIG. 2 is turned on after the release, the focus is continuously detected and displayed. In AF mode, see # 23 to see if it is single shooting mode or continuous shooting mode based on the DR signal. If DR = 0, it is single shooting mode, and in # 25, the AFE signal of the terminal (P12) is “High”. To This signal is for notifying the control microcomputer (MC2) that the automatic focus adjustment operation is completed and the focus is achieved and the release is possible.

When the shutter release button is pressed down to the second step, the control microcomputer (MC2) permits this release when it is "High" when it sees this signal in AF priority mode, and "Low".
If so, release is not allowed. That is, in the single-shot mode, after focusing and releasing once, keep pressing the release 1-step (switch (S1) ON), AFS
"AFSINR" from # 15 if no interrupts such as signals come in
, The AFE signal goes "High" at # 25.
If the position of the subject is changed as it is, for example, the shutter can be released in the out-of-focus state. At this time, the lens is not driven because it is waiting for the release interrupt or the AF microcomputer (MC1) stop interrupt at the next # 26. This sequence can be called "AF lock".

On the other hand, if it is the continuous shooting mode, the process proceeds from # 23 to # 24 to check whether or not the auxiliary light AF mode is in progress. In the auxiliary light AF mode, the continuous shooting mode and the auxiliary light AF mode are in effect, so automatic focus adjustment and release are allowed only once, and once released, the next release and automatic focus adjustment are prohibited.
Therefore, the AFE signal does not go "High" and the process proceeds to # 26. In continuous shooting mode other than fill-in AF mode
Proceed to "A" to enter the next focus detection.

The flow starting from “AF START” in # 33 of FIG. 9 starts from # 14. In # 33, the subroutine “SIOSE in FIG. 15 is displayed.
Calling "T". When starting the operation of the AF microcomputer (MC1), the control microcomputer (MC2) receives various data to determine the operation mode. The mode decided at this time is
It is automatically written to the mode register RG in the AF microcomputer (MC1). This register RG is for checking whether the mode has been changed later. In # 34 and # 35, the operation mode is checked, and if it is neither AF mode nor FA mode but MANUAL mode, proceed to # 36. # 36
Then, in case of another person, all the signals MR, MF and MB to the driver circuit (MDR1) are set to "High" to stop the lens motor (MO1). In # 37, interrupts other than INT1 and INT2 are stopped, and it loops to # 33 and repeats.

When in AF or FA mode, proceed to # 38 to initialize the CCD image sensor (FLM) and warm up the sensor. The interface circuit (IF1) is set to A by setting the IOS signal of the terminal (P20) to “Low” in # 39.
This is also to set the mode to input the signal from the F microcomputer (MC1) and to set the mode to integrate the output of the CCD image sensor (FLM). And the first
Go to # 44 in Figure 10. Here, first, the 1-cut shot flag (1-cut shotF in Table 5-1), that is, the integration time is 5
Clear the flag indicating whether it exceeds 0 ms.
In # 45, set the AFE signal output from the terminal (P12) to "Low". I'm doing this here because it keeps looping even after focusing. This is because if the AFE signal is in focus, "Hig
Since it is a signal that becomes "h", it is set to "Low" in preparation for the next calculation. Next, at # 46, the NB2 signal is output from the terminal (P23) and the integration of the CCD image sensor (FLM) is started. To do.
In # 47, the lens drive pulse count value EVTCNT for correcting the lens movement amount during focus detection calculation and integration described later is read and stored in the memory T1. At # 48, half of the maximum integration time of the CCD image sensor (FLM), 100ms, is set to 50ms. In Fig. 9, there is "CDINT" starting from # 40 in parallel with "CDINTA", and there is another flow up to # 53,
This is a flow for the function called "convolution integration", and a description thereof will be given later.

Continue from # 48 to "TLNTφ" from # 55. # 55 allows all interrupt routines. In # 56, check the NB4 signal coming into the terminal (P25), and
If it is n ", it is a signal that the CCD image sensor (FLM) has completed the integration according to the brightness of the subject, so the flow proceeds to" CDINT2 "of # 64. If it is "High", it means that the integration is continuing, so proceed to # 57 and check whether the maximum integration time initially set has elapsed. That is, # 48
See if 50ms set in step # 40, 40ms set in # 53, 50ms in # 61 or 150ms in # 62 set in the future, and if not, return to # 56 and repeat the loop. After the maximum integration time, proceed to # 58. 1-cut here
If the shot flag (1-cut shotF) is not "1", proceed to # 59 and set "1" to this flag. 1-cu when going to # 63
Since the t shot flag is "1", it is after passing # 59 or # 49. In # 60, it is checked whether the 200ms flag (200msF in Table 5-2) is "1". If it is not "1", the maximum integration time is usually 100ms, so the remaining 50ms of integration set in # 48 remains. 50ms for # 61
Set with and return to # 56 to check the NB4 signal. # 6
When it is 0 and the 200ms flag is "1" (this is set in the later flow and only under special conditions, the maximum integration time is set to 200ms), the integration set in # 48 Set the remaining 150ms of 50ms and go back to # 56, NB4
Check the signal.

If the output from the CCD image sensor (FLM) is obtained to a sufficient level, proceed from # 56 to # 64. Here, even if the output is not sufficient, the integration must be ended if the maximum integration time has passed, and that is the time when the process proceeds from # 58 to # 63. # 58
Then the 1-cut shot flag is "1" this time, so be sure to #
Proceed to 63, and from the terminal (P21) to the interface circuit (IF
Output the forced integration stop signal NB0 to 1). Then proceed to "CDINT2" from # 64. The steps from # 64 to # 67 are the flow of "renormalization integration", and the explanation is given later.

In # 68, interrupts other than INT1 and INT2 are prohibited,
This is to prevent interruption of timing when the data is taken in after this and timing is not wrong. Since INT1 and INT2 interrupts start from the beginning of the main flow, do not disable them. # 69 turns off the ST4 signal at the terminal (P13) by turning it "Low" when the auxiliary light LED (48) is on during CCD integration. # 70 pin (P20) IOS
The signal is set to "High" and the interface circuit (IF1) is switched to the data output mode. That is, the signals of NB4 to NB0 become lines for data transfer, and data can be sent from the interface circuit (IF1) to the AF microcomputer (MC1). Although 8-bit data is sent as data, it is sent in two steps in 4-bit parallel from NB3 to NB0, and the timing is taken by NB4.
High-order 4-bit data is sent when gh "and low-order 4-bit data is sent when NB4 is" Low ". AF microcomputer (MC1)
Recreates and sends the data sent separately to the upper and lower layers.

Therefore, first, the AGC data sent from the interface circuit (IF1) to the AF microcomputer (MC1) is shown in FIG.
Any of the numerical values (1 times, 2 times, 4 times or 8 times) of the gain determined in the AGC controller (406) (hereinafter,
AGC data) is sent, and this is AFed at # 71 in Fig. 10.
Take it into the microcomputer (MC1). By the way, after the integration of CCD image sensor (FLM) is finished, the timing when these data comes out is decided by the interface circuit (IF1), and AGC data must be taken in immediately after the integration is finished. AGC data is output for a certain period of time, and as soon as this is completed, pixel data of the CCD image sensor (FLM) is also sent at a certain timing. Just 72 hours after capturing this AGC data, # 72
As described in, the lens drive pulse count value EVTCNT at the end of integration is read and stored in the memory T2. It corresponds to # 47 at the start of integration.

Immediately after this, the pixel data of the CCD image sensor (FLM) is input at # 73 and saved in the memory of the AF microcomputer (MC1). The next # 74 is a subroutine that checks whether the lens being driven hits the infinity end or the closest end while driving the lens. (MO
1) Stop or reverse drive. The subroutine "CKLOCK" will be described later with reference to FIG. In # 75, serial communication with the control microcomputer (MC2) is received, and data for driving the lens is received. Even though I got the data once in # 33, I am doing serial communication again here because it does not pass through # 33 in the repeated loop, so if the conversion coefficient KROM for lens drive changes in the middle (depending on the lens Will change depending on the focus condition, zooming, etc.), and the data will change if the microcomputer operation mode changes, so to check this repeatedly #
There is a "SIOSET" on the 75. Then, in # 76, the focus detection calculation is performed using the data of the CCD image sensor (FLM) imported in # 73. With respect to this method, the defocus amount DF is obtained by the method already proposed by the present applicant in Japanese Patent Application Laid-Open No. 59-126517.

From # 77 to # 85, whether or not the brightness of the subject is lower than a predetermined level is checked to judge by looking at the level of AGC data. Here, when the brightness of the subject is below a predetermined level, it is called low light. In # 77, "1" is set in the low light flag (low light F in Table 5-2). In # 78, if the electronic flash device is attached to the camera and the auxiliary light switch (44) is closed, the AFFL signal sent by serial communication is "1", so proceed to # 80. .. That is, if the auxiliary light emission enabled state is set, the AGC data is doubled and 4 times when the maximum integration time is 100 ms.
When it is double or 8 times, it becomes a low light judgment and # 86 “MAIN
When the AGC data is 1x, the low light flag is cleared to "0" at # 85 and goes to # 86. In the mode with the maximum integration time of 200ms, all become low light and go from # 80 to # 86.

On the other hand, if the auxiliary light emission enabled state is not set, the process moves from # 78 to # 81. In the mode with the maximum integration time of 100 ms, when the AGC data is 4 times and 8 times, # 82, # 83, # 8
It becomes low light judgment through 6 and AGC data is 1 and 2
At the time of double, it moves from # 82 or # 83 to # 85 and clears the low light flag and goes to # 86. Maximum integration time is 200 ms
In the case of the mode, when the AGC data is 2 times, 4 times, or 8 times, the low light determination is made by going from # 84 to # 86, and when the AGC data is 1 time, going from # 84 to # 85 is done # 85 Clear the low light flag and go to # 86. Here, the determination of low light when the auxiliary light emission enabled state is set is 1 more than the determination of low light when not set.
It starts from a bright place. This is because if the subject has low contrast and low brightness, focus detection calculation is impossible,
It is very effective when giving up automatic focusing. In other words, if the auxiliary light emission enabled state is set, the focus detection in the auxiliary light non-use state is given up early, and the focus is detected immediately by immediately entering the auxiliary light use mode to enable the auxiliary light emission enabled state. If is not set, the focus detection of only the outside light is detected to the place where it can go anyway,
If the contrast becomes low and the brightness becomes low, the lens is retracted without automatic focus adjustment. In this embodiment, before giving up the focus detection, the lens is further extended or reciprocated to perform one reciprocating scan to search for a position having contrast. This will be described in the flow after "LOWCON" from # 165 in FIG.

In the present embodiment, the determination of the subject brightness is based on AGC data, but this may be based on the integration time. For example, among the flags used in this embodiment, the CCD image sensor (F
If the integration time of LM) is 50 ms or more, it will be 1-cut shot
You may use a flag.

Now, the "MAIN1" from # 86 in FIG. 11 will be described below, but from here, the process of driving the lens will be explained. First #
The 86 compares the serial data obtained in # 75 with the mode in which the AF microcomputer (MC1) has been operating so far, and if the mode has changed, restarts from "AF START" in # 33. That is, the contents of register RG indicating whether AF mode / FA mode / MANUAL mode set after the last serial communication # 33 or single shooting / continuous shooting mode and the focus detection mode flag (AF mode Flag, FA mode flag),
It means that if it is changed by comparing with the flag (DR) of the single shooting mode, the process proceeds to # 33. Then, at # 33, a new mode is automatically written in the mode register RG. In # 87, it is checked whether or not the mode is the focus detection operation mode using the auxiliary light. If it is the mode using the auxiliary light (hereinafter referred to as the auxiliary light AF mode), the focus of the auxiliary light in FIG. 14 is used. Detection flow # 238 "LSAV
Enter "E". Note that the method of entering the fill-in AF mode is that the subject is in a state of low contrast and low brightness. Therefore, enter from the low-contrast flow starting from “LOW CON” in # 165 of FIG. become.

If it is not the auxiliary light AF mode in # 87, the low contrast flag (current low contrast F in Table 5-1) of # 88 is checked in # 88 to determine whether or not the result of the focus detection calculation is low contrast last. If there is, the "L" of # 165 in Fig. 13
Move to "OWCON" flow. This time the low-con flag that appears in # 88 is identified and set in # 76. If the result of this operation is not low contrast, #
Proceed to 89, check the AGC data input in # 71 of FIG. 10, and if the AGC data is 1 time, clear the 200 ms flag in # 90. This is the maximum integration time when it was dark
I mentioned that there is a state of 200ms mode, but when it is in 200ms mode, if the AGC data is 1 time, it is not necessary to set it to 200ms mode, and it is better to set it to 100ms mode with a shorter maximum integration time. This is because the time is short. When integration time is 200ms and AGC data is 1 time, integration time is 100m
It can be seen that the pixel output is almost the same as when the AGC data is doubled in s, and it is disadvantageous when the integration time becomes long, considering the movement of the subject and camera shake. If you can find the contrast of the subject,
The maximum integration time is 100ms.

The flow of "NLOC1" starting from # 91 is a flow when the contrast is found in the subject, and in # 91, the scan prohibition flag is set to "1". This is because if the contrast of the subject is low, look for a high contrast position,
Focus detection while moving the focusing lens is called low-con scan. However, once the contrast appears on the subject, this low-con scan is performed in a series of sequences while the switch (S1) is closed. Is prohibited. Because, if you scan frequently, it is difficult to use as an autofocus camera, and the contrast was found once, so even if the focus is detected continuously in the vicinity of the current lens extension position, it will be low contrast. However, it seems that there is a high probability that the contrast will be found again, and even if the low contrast is reached next time, it is counterproductive to focus detection if the low contrast scan is started immediately.

Further, the reason why the scan is prohibited is that, in addition to this, there is a case where the scan is once completed with low contrast. The flow from # 92 to # 101 mainly shows the processing when a sufficient contrast is found during the low contrast scan. This can be roughly divided into two cases, and it is divided when the integration time of the CCD image sensor (FLM) exceeds 50 ms and when it is not. When the subject is dark such that the integration time exceeds 50 ms, when the contrast is found during low contrast scanning,
Once the lens is completely stopped, focus detection is performed again, and the lens is moved to the in-focus position according to the result. Focus is not detected while the lens is moving. The reason is that when the lens is driven when the integration time becomes long, the image of the subject flows out, which adversely affects the defocus amount calculation. Integration time becomes longer, and AG
This is because when the magnification of C becomes large, the noise due to the dark output variation of the CCD image sensor (FLM) also becomes large, and if the image flows in this state, delicate focusing will be lost.

Therefore, when the integration time exceeds 50 ms, the focus is not detected while moving the lens, and the focus is detected only when the lens is stopped. This is called the 1-cut shot mode. A flag indicating that (1-cut shot flag in Table 5-1) is provided. This flag is already set in # 49 or # 59. Next, in the case of a bright subject whose integration time does not exceed 50 ms, if sufficient contrast is found during low-con scanning, focus detection is performed using the contrasted data without stopping the lens this time. Calculate. The lens is driven to the resulting focal point. During this period, the focus detection calculation is repeated, and the lens drive amount up to the in-focus position is constantly refreshed for focusing. This is called the multi shot mode because the focus is repeatedly detected while the lens is being driven. When it comes to focus detection without stopping the lens during low contrast scanning, the lens position is different between the time when the CCD image sensor (FLM) is integrated and the time when the lens drive amount is obtained. For the preparation for correcting this movement, see “LO
It is performed in the "WCON" flow, and the movement amount is corrected using this. The idea about this movement correction is
Since it is described in Japanese Patent Laid-Open No. 59-68713, detailed description will be omitted here.

Next, find the contrast in the low contrast scan,
It is possible that low-contrast results may be obtained even after the operation of the multi shot mode is started. In this case, the result of low contrast is ignored, and the lens is driven to a position that is considered to be the in-focus point according to the drive amount set before the low contrast is obtained. Only the results with contrast are used for driving. The decision to exit the low contrast state is made by checking the previous low contrast flag (previous low contrast F in Table 5-2). This flag is set in the "LOWCON" flow from # 165 of FIG. 13, and is set when the previous calculation result was low contrast. On the other hand, when it comes to # 92, it means that there was contrast in this result, so # 92
Then, if the low contrast flag was set to "1" last time, it means that the low contrast was exited and the process proceeds to # 93. If the low contrast flag was “0” the last time, there is contrast from the beginning and it is passed as # 92 when the focus is detected.
To # 102. In # 93, the focus adjustment status display is turned off. Until now, when the lens drive was in a low contrast state and the lens drive was stopped, a blinking display indicating that focus detection is not possible is displayed, but this is erased because the contrast appears. In # 94, if the 1-cut shot flag is set as described above, it is necessary to stop the lens, so proceed to # 95. Do not stop, # 101
Go to. In # 101, the previous low contrast flag, the per-scan flag (F per scan in Table 5-1) and the in-scan flag (In-scan F in Table 5-1) are cleared. This is after finishing low contrast scan,
Alternatively, it is for resetting the flag indicating the state when the scan is in progress. Of course, the scan prohibition flag is left without being reset.

# 95 comes when it is in the 1-cut shot mode state, but here, by checking the scanning flag, it is checked whether or not it came during low-con scanning. If it is not scanning, proceed to # 101, go to the one that drives the lens according to the current calculation result, and if it is scanning, # 96, #
At 97, the lens drive motor (MO1) is de-energized and the brake is applied according to the signal pattern shown in Table 6. In order to remember the state where the lens is stopped, the driving flag (driving F in Table 5-2) in # 98 is cleared. At # 99, wait 70ms for the lens to stop completely. At # 100, clear the same flags as at # 101, return to "CDINTA" at # 39, and start the next focus detection. As described above, the # 99 wait time causes an image to flow if the lens is moving when the integration time of the sensor is long. Correct correction is difficult when a negative acceleration is applied. Therefore, if the next sensor integration is started after the lens is completely stopped, the focus shift of the focus detection calculation can be prevented.

Next, the flow for converting the defocus amount of the focus detection calculation result into the pulse count value for driving the lens "MPUL
There is an S ". In # 102, the defocus range in which the lens is in focus within this range is set in the register FZW as the focusing zone. Note that here, the focus zone amount in the automatic focus adjustment state (AF mode) and the focus zone amount in the focus adjustment display state (FA mode) are distinguished,
Set a wider value in FA mode than in AF mode. # 103
Since # 106 is the flow when the lens is stopped at the end, this is the case when the lens is hitting the end at infinity. The end flag of # 103 (end F in Table 5-2) is
It is made in the termination check subroutine before coming here. If the lens has stopped at the end, the process proceeds to step # 104, and the direction flag (previous direction F in Table 5-3) is checked to see in which direction the lens is about to move. If the lens is at the infinity end and you are trying to drive to the infinity side, proceed to # 105 to check the end position flag (end position F in Table 5-2) to see if the end position is at the infinity end side. Looking at the closest end side, if it is at the infinity end side, proceed to # 106 and set the focusing zone to a large value of 255 μm. If the lens stop position is the closest end, # 10
Go to 7 Even if the lens is at the infinity end position due to variations in the focus detection data, this may result in the in-focus position being further toward the infinity end, and if a narrow focus zone is set. , At the infinity end, there is a possibility to move the lens toward the infinity side. or,
Furthermore, the position at which the lens is considered to be at the infinity end may actually stop the lens midway due to other external stress. In the present example, this is indistinguishable.

Therefore, when the detection result shows that the lens is at the infinity end and the in-focus position is beyond the infinity end,
First, widen the focus zone to 255 μm, and if the lens is inside the focus zone, the focus display will be shown. If this value is not within the focus zone, focus detection is not possible (LED blinks) Display). If the lens is forcibly stopped by hand etc. while the lens is trying to move to the infinity side during automatic focus adjustment, the LED will blink if the lens stop position is not within the focus zone. That is. The flow of this display is from # 120 to # 123.

On the other hand, if there is a lens at the closest end and it is detected that the subject is on the close side, or if the lens is trying to move to the close side during automatic focusing, the lens is forcibly stopped halfway. If the position is not within the in-focus zone, the display is made in the closest direction. The flow of this display is from # 147 to # 152 in FIG.
Hit If the lens does not stop at the infinity end, the focus zone moves to # 107 with the value set in # 102.

In # 107, it is checked whether or not the auxiliary light AF mode is set based on the auxiliary light mode flag. If it is the auxiliary light AF mode, chromatic aberration correction is performed. Since the illumination light in the auxiliary light AF mode uses light having a wavelength close to infrared light, the best focus position is displaced due to the difference in light source during flash photography. Therefore, if the auxiliary light AF code is used, this focus position shift amount must be corrected. As shown in Table 4, the correction data ΔIR corresponding to the taking lens is sent from the control microcomputer (MC2) by serial communication. This is corrected in # 108 with respect to the defocus amount DF that has been obtained so far. Then, in # 109, the defocus amount is converted into a pulse count value for driving the lens. Since the coefficient for this conversion is also unique to each lens, the data KROM sent by serial communication is used like ΔIR. The defocus amount DF found is also multiplied by the conversion coefficient KROM to find the pulse count value DRCNT for driving the lens. Similarly, the focusing zone FZW is also multiplied by the data KROM and converted into the pulse count value FZC.
Regarding the conversion into these pulse count values, JP-A-59-14
Since it is described in detail in Japanese Patent No. 0408, it is omitted here.

Then, in # 110, it is determined based on the driving flag (driving F in Table 5-2) whether or not the automatic focus adjustment operation is currently being performed, and when the lens is driving, “IDOBU
Branch to N ”. When the lens was stopped, that is,
When passing through the flow for the first time, when confirming the in-focus position after completion of automatic focus adjustment, or when in FA mode, proceed to # 111. Here, the defocus amount DF when the lens is stopped is stored in the memory FERM.
Save to. This value will be used later to determine whether to go to the loop for checking the in-focus position after the end of automatic focus adjustment or not according to this value. In the next step # 112, it is determined whether or not the FA mode is set based on the FA mode flag. If the FA mode is set, the flow branches to “FAP” from # 113. This is because the non-AF mode is the FA mode.

In # 113, it is judged whether or not the lens is in the focusing zone. Here, the lens drive pulse count value DRCNT and the focus zone pulse count value FZC are compared, but the defocus amount DF and the focus zone amount FZW may be compared. As a result, if there is a lens in the focus zone, focus display is performed in # 115. This is the terminal (P31) LM
This is done by setting the signal to "Low", leaving the LL and LR signals at "High", and turning on only the central LED (LEDM). If it is outside the focusing zone, the process proceeds to step # 114 where the direction in which the lens should be driven is shown. For example, in the lens extension direction, set the LL signal of the terminal (P32) to "Low" to turn on the left LED (LEDL), and in the lens extension direction, set the LR signal of the terminal (P30) to " Set to "Low" and light the right LED (LEDR). Then, for the next focus detection, it loops to "CDINTA" of # 40 in FIG.

If it is in AF mode in # 112, focus check in AF mode is performed in # 116. Lens drive pulse count value DR
If the CNT is smaller than the focus zone pulse count value FZC, it means that the focus is achieved, and the process branches to “INFZ” from # 117. # 1
In 17, the focus display is displayed as in # 115 in FA mode, and
At 18, set the AFE signal from pin (P12) to "High". The control microcomputer (MC2) is watching this signal, and if it becomes "High", it is considered that the automatic focus adjustment has been completed. Then, in the AF priority mode, the release operation becomes possible only after the AFE signal becomes "High". In # 119, you will be waiting for the AF stop INT1 interrupt or INT2 release interrupt here. This is the switch (S
1) This is a method when the one-shot mode is used, in which automatic focus adjustment is performed only once when the subject is closed once. Once the subject is in focus, the focus is displayed even after changing the focus position. The lens will not be driven again. Also, as another method, instead of waiting for interrupt at # 119, if you return this to “CDINTA” of # 39 or “CDINT” of # 40, focus detection will be repeated and automatic focus adjustment will always follow the subject. You can also set it to continuous mode.

When it is determined that it is out of the focusing zone in # 116, # 120
Go to. As described above, here, the termination flag (the 5-2nd
It is the end by checking the end F) of the table (# 120), the previous position flag is checked and the focus position of the focus detection result is at the infinity end side (# 121), and the lens stop position is at the infinity end. If it is (# 122), proceed to # 123, do not drive the lens, blink both LEDL (LEDL) (LEDR) on both sides to indicate that focus detection is impossible, and wait for interrupt at # 119. , I will not go to the next focus detection. In cases other than these conditions, the process proceeds to # 124.

From # 124 to # 130, the reversal check of the defocus direction is performed. That is, by comparing the defocus direction of the previous focus detection calculation result with the direction of the result calculated by this loop, if it is found that the defocus direction is reversed, correct the backlash of the lens drive system. That is. In driving the lens,
In particular, a considerable amount of play is provided in the coupler portion of the driving force transmitting shaft between the camera body and the lens. Therefore, if the lens driving direction is reversed due to a change in the distance to the subject, the lens will not move to the in-focus position determined by the calculation result due to the amount of rotation from the motor (MO1). Therefore, if the direction is reversed, the amount of backlash must be corrected. This backlash amount is unique to the taking lens, and as shown in Table 4, the control microcomputer (MC2)
It is obtained by serial communication from. However, when the previous defocus direction that appears here is the first loop after closing the switch (S1), remember that this is also the last lens drive direction in the previous sequence. ing. That is, the memory is remembered even in the stop mode of the microcomputers (MC1) (MC2) before the switch (S1) is closed. Further, this backlash correction is not so right after the calculation result is reversed, but this correction is limited only when the lens is stopped. If the result is that the direction is reversed while driving the lens, just stop the lens and do not immediately perform the reverse driving of the lens. Also, the previous direction flag is not reset. Therefore, the direction (current direction) obtained by the next focus detection calculation after stopping the lens is the direction that was obtained once before the lens was stopped, that is, the direction that was driving the lens. If it is reversed from (previous direction), it means that the backlash will be corrected for the first time. This is because the dispersion of the calculation near the in-focus position is taken into consideration so that the lens does not cause hunting due to the error of the backlash amount.

The flow for these is # 124 to # 130, which will be described below, and # 134 in FIG. 12, which is the flow during lens driving.
Has been achieved in combination with # 140. In # 124, the current direction flag (current direction F in Table 5-3) is checked to see the current defocus direction, and in # 125 and # 126, the previous defocus direction is checked. If the defocus direction is different between the last time and this time, # 127,
Go to # 128 and rewrite the previous direction flag.
If they are in the same direction, skip to "TINNZ" in # 141. #
In 129, the backlash correction data BKLSH sent by serial communication is corrected with respect to the lens drive pulse count value DRCNT, and in # 130, the reverse flag is used to reverse and correct the backlash (Table 5-2). F) is set and the process proceeds to step # 141.

Next, with reference to FIG. 12, the flow "IDOBUN" from # 131 when the lens branched from # 110 is being driven will be described.
At # 131, check if the lens is hit at the end, and at # 132, read the event counter value EVTCNT for the third time to correct the movement amount and register it.
Store in T3. Now you have all the data for the correction of the movement. That is, T1 at the start of sensor integration, T2 at the end of integration, and T3 at the end of focus detection calculation, using these three values, focus detection calculation based on pixel data obtained by integration during lens driving. As a result, the amount by which the lens moves until the lens drive amount is set after the actual calculation is completed is corrected. When the moving amount Tx of the lens during integration is calculated by the pulse count value, Tx = T1
−T2. Since the event counter is a subtraction count here, T1> T2 and Tx is positive. The amount of lens movement Ty in the time required for focus detection calculation is Ty =
Calculated as T2-T3. Assuming that the lens is moving at a constant speed, the intermediate position of the sensor integration time is represented as the point where the subject data was obtained. Tz = Tx / 2 + Ty The lens has moved by the amount of. Therefore, if Tz is subtracted from the count value DRCNT obtained by the calculation result of this time, the movement amount is corrected. So, in # 133, D
RCNT-Tz is newly replaced as DRCNT, and the value is set as the next lens drive pulse count value.

Steps # 134 to # 140 are the flow when the defocus direction is reversed during lens driving as described above. In # 134, the current direction flag is checked to see the current defocus direction. Check the previous direction flag to check the previous defocus direction, and if the direction is reversed, proceed to # 137. If not reversed, proceed to # 141. #
In 137 and # 138, the lens drive motor (MO1) is de-energized and the brake is applied to stop it. In # 139, the driving flag indicating that the lens is being driven is cleared, and in # 140, wait 70 ms until the lens stops. Then proceed to # 39 "CDINTA".

“TINNZ” starting from # 141 is a flow that merges from both during lens driving and during lens stopping, and is a part where the lens driving pulse count value DRCNT is set and the lens is moved. The driving speed of the lens is a two-stage type in this embodiment, and it is set to switch between high speed when the lens is far away from the focus position and low speed near the focus position of the lens. . The part that controls the lens at low speed is called the near zone. In # 141, the lens drive pulse count value DRCNT
However, if the lens is within the near zone area, the process proceeds to step # 143, where the near zone flag (near zone F in Table 5-2) is checked. ), # 144
Then, the MC signal from the terminal (PO3) is set to "Low" to drive the lens drive motor (MO1) at low speed as shown in Table 6. On the other hand, when outside the near zone,
Proceed to # 142 to set the MC signal to "High" to drive the lens drive motor (MO1) at high speed.

Although a part of the description has been given in the above, from # 145 to # 152 is a flow of processing when the lens is stopped at the end position. By the way, detecting that the lens is stopped at the end does not mean that there is a switch at the lens end position, as described in the subroutine from "CLOCK" in Fig. 14 below, and it is input from the interrupt port INT3. It is judged that the lens is stopped when the pulse from the motor drive amount monitor encoder (ENC) is not input for a certain period. If the lens is stopped even though the motor (MO1) is being driven, it is judged that it is hit at the end of the lens, and "CLOCK"
In the sub-routine, the motor drive is stopped and the end flag is set. With this method, even if the lens is not at the end, it will be forcibly stopped in the middle, or something will be caught in the lens, or the lens will stop for a moment (on the order of several 100 ms). Even if you see that the lens has stopped at the end to prevent such a thing, try moving the lens again, and it will be judged as the end by the "CLOCK" subroutine again,
It is said that it actually stops at the end. The flag to see this is the end 2nd flag (end 2F of Table 5-2), and # 145
Then, look at the end flag created in the "CLOCK" subroutine, and when it is "1", look at this end 2nd flag in # 146. In the initial state, this flag is "0", so proceed to # 150, set the 2nd end flag,
The lens drive flow from 153 moves the lens. Then, when it comes to # 146 in the next loop, it is judged that the vehicle has stopped at the end for the first time, and the process proceeds to # 147.

In # 147, the current defocus direction is checked, and in # 148 and # 149, the end position flag is checked to see which side the lens is currently hitting. That is, assuming that the current defocus state is the front focus (current direction flag = 1) and the lens position is at the infinity end,
The lens will have to be moved further to the infinity side than the current infinity end. In this case, # 148 to # 4
Go to 0, and in the next loop from "CDINT", expand the focus zone and check the focus again as described above.

This time the defocus state is the rear pin (this time direction flag =
0), and if the lens position is the closest side (end position flag = 1) in # 149, the lens must be moved to the closer side. In this case # 14
Proceed from 9 to # 152, and set the LL signal from the terminal (P32) to "Low".
Then, the direction indicator for instructing to move the lens to the closest side is turned on. Then leave the lens stopped,
Go to the next loop from # 40 and repeat focus detection. Then, if the position of the subject changes and the defocus direction is reversed, the process proceeds from # 147 to # 148 in the loop, goes to # 151, clears the end flag, and enters the lens drive loop from # 153. In this embodiment, the current direction flag is used for checking the defocus direction of # 147, but the previous direction flag may be used. In this case, the lens is moved from the state where the subject is closer to the closest end than The lens does not follow and remains stopped even if it enters the focusable area of. In the case of the one-shot AF mode, the latter method is sufficient, and in the case of the continuous AF mode, it can be said that it is not the former.

In this latter case, once the low contrast state is reached, the termination flag is cleared in the "LOWCON" flow of # 165 in Fig. 13, so the lens exits from the closest edge and enters the lens drive state again. Entering, it means that automatic focus adjustment is possible. Next, if the lens is not at the end or if it is at the end but is about to move in the opposite direction, the lens drive flow from # 153 in FIG. 12 is entered. In # 153, all focus adjustment status display LEDs are turned off. This is based on the basic principle that the defocus direction is not displayed while the lens is being driven. When the lens is stopped, the center LED (LEDM) is lit to indicate the focus when the lens is in focus, and either LED (LEDL) (LEDR) is lit to display the defocus at the closest end or the infinity end. The focus direction is displayed, and the LED (LEDL) (LEDR) blinks when the contrast is low. In # 154, the lens drive pulse count value DRCNT is set in the event counter EVTCNT and the termination check register MECNT. Value set in event counter EVTCNT
DRCNT is subtracted in this interrupt flow (INT3S in Fig. 16) when a pulse from the encoder (ENC) enters the interrupt terminal (INT3) and interrupts the AF microcomputer (MC1). The mechanism is that if the lens is stopped when the count value DRCNT reaches “0”, the image is in focus.

In # 155, the lens driving motor (MO1) is energized to start lens driving. This moves the lens according to the previous direction flag. That is, this flag remains as the lens driving direction so far. Because the previous direction flag, when the lens is stopped,
This is because the content from the current direction flag is the same as the flow from # 124 in FIG. If the previous direction flag is "0" (rear pin), the MF from the terminal (P01)
Set the signal to "Low" and extend the lens as shown in Table 6. If the previous direction flag is "1" (front pin), set the MR signal from the terminal (P00) to "Low" and extend the lens. Move in the direction. In # 156, the driving flag is checked to see if the lens has been driven so far. If it is driving (explained later, driving here means automatic focus adjustment outside the near zone. (Middle), loop to # 40 [CDINT] and enter the next focus detection. If the lens has been stopped so far, the driving is started in # 155, so the driving flag is set in # 157. At # 158, the auxiliary light mode flag is checked to see if it is the auxiliary light AF mode. If it is the auxiliary light AF mode, the process branches to "L2SAVE" from # 231 in FIG. If it is not the auxiliary light AF mode, check whether or not the lens is driven in the near zone by checking the near zone flag at # 159, and if it is in the near zone, proceed to [WSTOP] from # 160. # 160, #
The 161 simply repeats the end check at 100 ms intervals and does not return to the next focus detection loop. Then, it waits until the lens completely stops at the in-focus position, waits for the lens to stop, and then starts focus detection for in-focus confirmation. This is "WSTO
While turning the "P" loop, "INT3" of # 252 in Fig. 16
The "S" interrupt comes in and controls the lens.

The reason why focus detection is not performed while driving the lens in this linear zone is as follows. First, the lens drive in the near zone has acceleration rather than constant speed. That is, the lens has a positive acceleration at the start of driving the lens and has a negative acceleration before the lens stop position. When entering the near zone from high speed driving and switching to low speed, it has negative acceleration. Here, originally, the near zone count amount NZC is determined based on the count value from high speed to when the motor (MO1) is de-energized and the movement of the lens stops. The motor (MO1) is constant speed. It is not an area for movement. Here, the fact that the speed is not constant means that even if the sensor is integrated while the motor is being driven, it cannot be represented as the point at which the subject data was obtained at the intermediate position of the integration time. Therefore,
Even if the correction for the movement amount as described above is made, the correction is not accurate and has a calculation error of the lens driving pulse.
Therefore, it is desirable not to integrate the sensor when the lens is not moving at a constant speed. Therefore, in this embodiment, focus detection is not performed during acceleration or deceleration.

Next, when # 159 is judged to be outside the near zone, # 1
It branches to 62 and waits for 100ms here. Since the lens is accelerating from the stopped state, it waits for 100 ms until the speed becomes constant. Then, the end check is performed at # 163. The end check cycle may be too short or too long. If it is shorter than the encoder pulse interval according to the movement of the lens, it will be judged that it has stopped, and if it is too long, the durability of the drive system such as the motor, gear, clutch, etc., and the reaction drive at the end Since there are problems such as the responsiveness of, the interval is set to several tens to 200 ms. Next, in # 164, it is checked whether the 1-cut shot mode is set by looking at the 1-cut shot flag. In the 1-cut shot mode, focus detection is not performed while driving the lens. So # 160
Go to "W STOP" to wait for the lens to stop, and then stop and perform focus detection for confirming focus. 1-cut
If it is not shot mode, loop to # 39 "CDINTA" in FIG. The above is the main routine of automatic focus adjustment.

Next, the branch routine and the subroutine from FIG. 13 will be described. First of all, "LOWCO
The “N” flow is a flow that branches from # 88 of the main routine of FIG. 11 when the result of the focus detection calculation is low contrast. First, in # 165, the terminal end is checked, and in # 166, the AF mode flag is checked to see whether or not the AF mode is set. If it is not in AF mode, proceed to # 167, set the low contrast flag last time, and repeat the low and high LL and LR signals of the terminals (P32) and (P30) at the same time as the low contrast display in # 168. LED (LEDL) (LED
R) blinks. Then it immediately loops to the next focus detection. In AF mode, proceed from # 166 to # 169,
Check if the motor is driving by checking the driving flag. If it is driving, there may be a case where low contrast scanning is in progress and a case where low contrast has been obtained during automatic focus adjustment. If the focus is being adjusted, the result of low contrast is ignored until the lens is stopped, as described above, so the process immediately proceeds to # 40 "CDINT" to start the next focus detection. # 170 during low contrast scan
If you come to # 171, get out of the low contrast state at # 171 and adjust the event counter value T3 at the end of calculation to the maximum count value 65,000 in order to correct the movement amount during renormalization integration when starting automatic focus adjustment. Set to. (Details will be described later) Similarly, motor drive event count value
EVTCNT, end detection count value MECNT also has maximum count value 6
Set it to 5,000. And it loops to "CDINT" of # 40.

If the contrast is low when the lens is stopped, proceed from # 169 to # 172. Then, if the scan prohibition flag indicating prohibition of the low contrast scan is set, the process proceeds to # 173. It should be noted that the fact that the scan prohibit flag is delayed means that either the low contrast scan has already been completed once or the contrast has been generated.

Steps # 173 to # 175 and # 181 to # 183 are steps in which it is determined whether or not the auxiliary light AF mode is entered. The conditions for entering this auxiliary light AF mode are that it is first in AF mode, that the subject has low contrast, that the lens is stopped and that it is low light, and that the auxiliary light shown in FIG. It means that the electronic flash device equipped with the lighting device is attached to the camera, the AFFL signal indicating that the auxiliary light can be emitted is coming, and the charging completion signal RDY is also coming. Enter auxiliary light AF mode. First # 17
3 for low light flag, # 174 for fill light OK signal AFFL, # 17
When you see the charge completion signal RDY at 5, if all the conditions are "1", jump to "LLLED" from # 225 and enter auxiliary light AF mode. If this condition is not met, the low light state is checked based on the low light flag in # 176, and if it is low light, the maximum integration time of the sensor is doubled to 200 ms in # 177. AGC is 8 times with integration time of 100ms, low contrast,
This is because, in the case of low light, if the integration time is increased by one step, the low contrast may not be achieved and focus detection may be possible. However, because the error of focus detection while driving the lens is generated when the integration time is long, the maximum integration time is set to 200 ms mode only when the lens is stopped.

In # 178, the previous low contrast flag was set, in # 179, the LED (LEDL) (LEDR) indicating the low contrast state was blinking, and in # 180, the near zone flag and renormalization integral flag (renormalization integral F in Table 5-1). ), Clear the inversion flag, end flag, and end 2nd flag, and loop to "CDINT" of # 40.

If the low contrast scan is not prohibited in # 172, the flow branches to "SEARCH" from # 181. The flow from # 181 to # 195 is a flow for starting the low contrast scan. First, in steps # 181 to # 183, the conditions for entering the auxiliary light AF mode are determined in the same manner as in the flow from # 173 to # 175. Then, if the conditions are met, it jumps from # 183 to #LLLED of # 225 and enters auxiliary light AF mode. If it is low-ride, but the auxiliary light illuminator is not set and the AFFL signal is not "1", proceed from # 181 to # 182 and # 184, where the maximum integration time of the sensor is already 200ms. Check if it is in mode.

If it is not in the maximum 200ms mode, jump to "LL200" of # 230, set the 200ms mode flag and # 39.
Loop to "CDINTA". # 184 already up to 2
If it is low contrast even if it is in the 00ms mode, or if it is low contrast in # 181 but not low light, proceed to # 185 and clear the 200ms mode flag.

This is because if the integration time is long during low-contrast scanning, the image of the subject tends to flow as described above, causing low contrast, and even if there is contrast, the integration time and focus detection If the maximum calculation time is reached, it is possible to have a lens with a large drive ratio, in which the lens has stopped, and when the focus is detected again, it has already gone too far beyond the in-focus range. For this reason, the 200ms mode flag is cleared and the maximum integration time is set to 100ms.

Next, in the flow from # 186 to # 190, the method of starting the scan of the lens at the time of low contrast scan is determined. When the subject is bright, the low contrast scan starts scanning from the direction determined by the focus detection calculation.
Even if it is determined that the contrast is low and the defocus amount is not obtained, it may be obtained in the defocus direction, so scanning is performed according to the direction of the calculation result. If the area where the defocus amount is obtained during the low contrast scan comes, the automatic focus adjustment operation starts as described above. In the low contrast scan, if the lens is at one end, it is driven in reverse, and if it is at the opposite end, the scan ends. Whether the object is dark or bright is checked using the 1-cut shot flag which indicates whether or not the integration time exceeds 50 ms in # 186. For this, AGC data may be used, and the darkness may be 2 times or more, or 4 or 8 times or more. On the other hand, when it is dark, the process proceeds to # 187 to start the low contrast scan from the feeding direction. In this way, the final stop position at the end of the low-con scan ends with the lens retracted at the infinity end. This means that when the lens is capped, it will end in the retracted state, and the lens will be compact and convenient for storage in the camera case.

At this time, if the function of ending the lens by retracting the lens is emphasized instead of the purpose of searching for the contrast, the process may proceed to # 187 “LLIGHT2” without proceeding to # 187. That is, in # 189, a per-scan flag (F per scan) indicating that the low-conscan has hit the end once is set.
At 190, set MR signal to "Low" and start low contrast scan in the renormalization direction. When the lens hits the far end, ignore # 189
In the "ROTEM" from # 199 in FIG. 14 determined by the per-scan flag, it is determined that the scan is completed, and the lens is stopped. In addition, this "LLIGHT2" is where you fly from within the auxiliary light AF mode flow.

In # 191, the low control flag is set to "1" last time, and in # 192, the scanning flag is set. In # 193, the maximum defocus amount FERM when the lens is stopped is set to 65,000. Similar to # 171 in # 194, maximum value of 6 for T3, EVTCNT, MECNT
Set 5,000. When driving the lens in # 195, the display is turned off. Then, while scanning, the process returns to the next focus detection loop # 40.

Next, the explanation will be given on the termination check subroutine "CKLOCK" in FIG. In # 196, it is checked whether the lens is being driven by looking at the driving flag, and if it is not driving, the end is not checked and the process returns. While driving the lens, proceed to # 197 to check the end. The end check register MECNT set with the same value as the lens drive pulse count value DRCNT during driving is compared with the count value EVTCNT of the event counter set as the lens drive count value DRCNT. If the lens is moving, EVTC
The NT value is decremented by 1 each time a pulse from the encoder (ENC) comes in, and is a different value from MECNT. If the lens does not move at the end,
No pulses come from the encoder (ENC), so EVT
The value of CNT does not change and remains the same value as MECNT. Therefore, if MECNT = EVTCNT in # 197, it is determined that the lens is stopped, and the process branches to # 199 in the termination processing flow “ROTEM”. If MECNT ≠ EVTCNT, it is determined that the lens is moving, and the process proceeds to # 198. In # 198, EVTCN changed to MECNT
Reset the value of T to prepare for the next termination check. Then return.

In the termination processing flow "ROTEM" from # 199, the subroutine is branched first, so the stack pointer of the microcomputer is reset. Disable interrupts other than INT1 and INT2 with # 200. Since it hits the end, the power is cut off to the motor (MO1) at # 201 and # 202, and the brake is applied. In # 203, the motor (MO1) is stopped, so the driving flag is cleared. Check the previous direction flag in # 204, and if the previous direction flag is "0" (it was the rear pin and the lens was extended), it means that it stopped at the closest end position in # 205, which means the end position. Set "1" in the flag. If the direction flag was "1" the last time (it was the front pin and the lens was retracted), the end position flag is cleared in the meaning of stopping at the infinite end position at # 206. In # 207, it is checked whether or not the end is hit during the low contrast scan, and if it is in scanning, the process proceeds to # 208, and the end flag that the lens is stopped at the end is set. In # 209,
Furthermore, based on the fill light mode flag, it is checked whether or not the fill light AF mode is in progress, and if it is in fill light AF mode, even if it is the focus detection by the first flash even if it hits the end, Instead of looping to the focus detection of, the LED blinks and the focus detection is given up. The auxiliary light AF mode will be described in detail in the "LLLED" flow from # 225. If it is not in the auxiliary light AF mode with # 209, the next focus detection loop "CD
Go to INTA ”.

In # 207, if the lens is at the end during the low contrast scan, proceed to # 210 to check if it has hit the end during scanning, that is, whether it is going or returning, If there is, it is necessary to reverse the scanning direction and move it, so proceed to # 217. # 217, this time
Since it has reached the end, the per-scan flag is set. Next, in # 218, the previous direction flag (indicating the lens driving direction) is checked, and in # 219 and # 221, the directions are reset in the opposite directions. Then, in # 220 and # 222, the lens drive signal MR or MF is set to "Low" according to the next moving direction. At this time, of course, the brake signal MB is set to "High". With this, the inversion drive is started. # 2
23, FERM, T3, EVTC
Reset NT and MECNT to the maximum value of 65,000 respectively. In step # 224, the driving flag is set to "1" and the process goes to the next focus detection loop "CDINTA".

On the other hand, if it has already hit the end and it was the second end, proceed from # 210 to # 211. This time, the lens does not move because the low contrast scan is completed. # 211 clears the per-scan flag that hits the end of the scan, # 212 clears the in-scanning flag, # 2
In the case of 13, the scan prohibit flag is set because once scanning is done, the rest is not done. In # 214, I did a low contrast scan, but I could not find the contrast,
Since the focus could not be detected, the LED blinks. In # 215, it is checked whether or not the auxiliary light AF mode is in effect. If it is in the auxiliary light AF mode, go to # 216 and wait for an interrupt without going to the next focus detection and end as it is. If it is not the fill light AF mode, focus detection is repeated at the end position after scanning is completed.
Return to TA. The above is the end detection routine.

Next, the auxiliary light AF mode routine will be described. Auxiliary light AF
The mode is entered from the "LOWCON" routine in Figure 13. If the above conditions are met, the process proceeds from # 175 or # 183 to "LLLED" in # 225, and the auxiliary light AF mode flow is entered. In # 225 of FIG. 14, first, an auxiliary light AF mode flag indicating the auxiliary light AF mode is set. In # 226, set the signal from the terminal (P13) to the terminal (ST4) to "High". The flash circuit (FLS) causes the auxiliary light LED (48) to start emitting light in response to this signal. In # 227, the LL and LR signals are set to “Lo” to notify the outside that the auxiliary light AF mode has been entered.
w "and turn on the LEDs (LEDL) (LEDR) at both ends. The lighting time is up to the end of the next focus detection calculation, up to 45
It is standard to turn on for 0 ms. This is the total time when the # 229 waits for 200ms, the calculation time for focus detection, and the maximum integration time is 200ms. To do. That is, this is also because the display is turned off while the lens is being driven. This display is only once when the auxiliary light AF mode is entered. On the other hand, the auxiliary light LED (48) emits light twice.
The auxiliary light AF mode sequence starts with the auxiliary light LED (4
8) emits light once and the CCD image sensor (F
Preliminary lighting for LM). This is to improve the responsiveness of the CCD image sensor (FLM). And
Mode with maximum integration time of 200 ms, C under fill illumination
Integrate CD. Then, the focus detection calculation is performed based on this data, and the lens is driven. During this time, focus detection is not performed. And after stopping the lens, the second LED for auxiliary light (48)
After a maximum of 450 ms as in the first time, if the focus detection result is not within the focus zone, the lens is driven again to perform focus adjustment. This is the basic movement.

Here, it is necessary to distinguish whether the auxiliary light LED (48) emits light for the first time or for the second time. In order to distinguish this, an auxiliary light 1st flag (auxiliary light 1stF in Table 5-2) is provided. If "0" is entered in this flag, it indicates that the first light emission has occurred, and if "1" indicates that the second light emission has occurred. #
In 228, put "0" in this flag. In # 229, wait 200 ms as the preliminary illumination time of the sensor, and set in 230 the mode in which the maximum integration time of the sensor is 200 ms. Auxiliary light A
In F mode, the integration time is usually 200ms. Then, it loops to "CDINTA" as in normal AF mode.

The flow proceeds from # 39 in FIG.
Turn off the auxiliary light at # 69 in the figure. The focus is detected in the same way, and the 13th
At # 87 in the figure, the flow branches to the auxiliary light AF mode flow “LSAVE” in # 238 in FIG. This is the flow starting from # 238.

First, it is determined whether or not the focus detection in the auxiliary light AF mode is the first time, and if it is the first time, the process proceeds to # 239. Here, it is checked whether or not the focus detection calculation result has a low contrast, and if the result is low contrast, “LLI
GHT2 ”and give up the second focus detection. After this, the process loops from # 189 and # 190 in FIG. 13 to # 40 in FIG. Since this is giving up and refilling, the auxiliary light is not emitted, so there is no need to go through the focus detection loop, but if you do this, if suddenly brightening and contrast appears during focusing, focus without the auxiliary light This is because it can be detected. If the contrast is not low in # 239, go to [NLOC1] in # 91 in FIG. 11 and enter the flow for focus adjustment drive. In this case, go through # 91 to # 102 in FIG.
Further, the drive starts at # 155 through # 141 in FIG.
It branches from 8 to the flow "L2SAVE"(# 231 in Fig. 14) in auxiliary light AF mode.

In # 231 of FIG. 14, it is checked whether or not the emission of the auxiliary light is the first time based on the auxiliary light 1st flag, and if it is the first time, the process proceeds to # 232. Here, the lens is driven by the count amount of the focus detection calculation result, and after the movement of the lens is stopped, the process proceeds to the second auxiliary light emission flow # 233. In # 233, see the fill light OK signal AFFL, and if it is “1” (OK), #
At 234, the second auxiliary light emission signal is output (that is, the signal at the terminal (ST4) is set to "High"). If the AFFL signal is "0", the auxiliary light illuminator has been turned off, so the second light emission is not performed. In this embodiment, the auxiliary light AF mode is not released in this case, but it may be released.

# 235 sets the auxiliary light 1st flag, and the second auxiliary light
Show that it is in AF mode. And like the first time, wait 200ms at # 229, go through # 230, and go to # 39 “C
Go to "Dinta". In the case of the auxiliary light AF mode in the second auxiliary light AF mode, the same flow is followed, through # 39 in FIG. 9 to # 44 and # 68 in FIG. 10, and in # 87 in FIG. To branch to “LSAVE” in # 238 of FIG. This time is the second auxiliary light AF mode, so proceed to # 240. Check whether it was low contrast at # 240, if it is low contrast, proceed to # 211, this time unlike the case of the first time, without stopping the lens, keep it stopped,
The LEDs (LEDL) (LEDR) on both sides are displayed blinking, and the system waits for an interrupt.

If not low contrast, # 240 to # 91 in Fig. 11
Proceed to and enter the lens drive flow. And in Figure 12 #
Branch to "L2SAVE" in the auxiliary light AF mode flow until 158. In # 231, it is the second auxiliary light AF mode, so # 2
Proceed to 36 and wait for the lens to stop like the first time. If it is not the auxiliary light AF mode, focus detection for focus confirmation is then entered, but since the emission of auxiliary light is limited to two times, focus detection for confirmation cannot be performed. (In this embodiment, since the light is emitted up to twice, the following processing is performed without confirmation. However, the number of times of light emission is not limited, and light may be emitted until the focus is confirmed. This process checks the focus detection calculation value FERM when the lens is stopped. That is, if the defocus amount at the start of the second lens drive is less than 1 mm, it is determined that the lens can be brought into the focus zone without sufficiently confirming the focus, considering the focus detection performance. In Step # 117 of Fig. 11, the flow for focusing is proceeded to "INFZ" to display the focus. If the FERM is 1 mm or more, the result of the focus detection for the first time and the focus detection for the second time are significantly different. Therefore, assuming that reliable focus detection could not be performed, proceed to # 211 and leave the lens at the current position. LEDs on both sides (LED
L) (LEDR) blinks. The above is the auxiliary light AF mode routine. Limiting the light emission of the auxiliary light LED (48) to two times is that power consumption and usage problems occur when the number of times of light emission is large, and focus detection error and backlash error occur when it is once. Therefore, the two times are appropriate. If the second focus detection is not possible, the lens is not retracted. If you open the switch (S1) once and then close it again and try the auxiliary light AF mode again, This is because there is a high possibility that the subject will start near the in-focus of the subject, and the possibility of bringing the lens in the in-focus zone will increase.

Next, the event counter interrupt flow "INT3
Let's start the explanation about "S". This is an interrupt pin (INT
3) The lens drive control is performed using the pulse signal PS from the encoder (ENC) of the lens drive motor (MO1) that enters. The drive count value EVTCNT of the lens up to the in-focus position was obtained by focus detection calculation. The interrupt signal to INT3 constantly monitors the lens drive amount, and controls the lens moving speed and stop position. First, the drive count value EVTCNT is set in the event counter when the lens is driven. Then, the energization of the lens driving motor (MO1) is started. Then, the lens starts to move, a pulse is output from the encoder (ENC) and INT3 is interrupted. And the flow of "INT3S" of # 252 starts.

First, the count value EVTCNT of the event counter is decremented by "1" because the "1" pulse signal comes at # 252. Then, in # 253, it is checked whether or not this count value EVTCNT has counted the specified amount (that is, "0"). If EVTCNT becomes "0", it means that the lens has come to the in-focus position and the process proceeds to # 259. , Stop the drive of the motor (MO1).

If the count value EVTCNT of the event counter is not "0", proceed to # 254 to check whether the lens is in the near zone based on the near zone flag. If the near zone flag is not "1", proceed to # 255,
I will check to see if I entered the near zone with this pulse. If the count value EVTCNT of the event counter is smaller than the count value NZC of the near zone counter at # 255, it means that the player has entered the near zone this time, and the process proceeds to # 256. If it is outside the near zone, it returns from the interrupt flow of "INT3S" to the main flow. On the other hand, in # 256, the near zone flag is set for the first time this time, so the near zone flag is set, and in # 257, the MC signal from the terminal (P03) is set to “Low”, and the drive of the motor (MO1) is switched to low speed. . Then, in # 258, the stack pointer of the interrupt flow is reset and the process proceeds to “WSTOP” in # 160 of FIG. 12 to wait for the lens to stop while checking the end.

That is, while looping through this "WSTOP" flow, "INT
3S ”interrupt enters, the flow from # 252 to # 254, # 258 is repeated, and when the count value EVTCNT becomes“ 0 ”,
Exit this loop and proceed to # 259. If it is in the near zone, the process goes to # 160 “WSTOP” and does not return to the main flow, because the focus is not detected when the lens is not moving at a constant speed as described above. Since the lens decelerates, it is not a constant speed, so if it enters this area, focus detection is not performed while moving the lens.

Next, when the lens has moved by the drive pulse count value EVTCNT, the count value EVTCN is checked by checking in # 253.
Since T becomes "0", proceed to # 259. Here, the lens drive motor (MO1) is de-energized, the brake is applied at # 260, the driving flag is cleared at # 261, the event counter interrupt is disabled at # 262, and the process goes to # 263. move on. Here, check whether it is in auxiliary light AF mode,
If it is in the auxiliary light AF mode, it returns from this event counter interrupt. This return destination is auxiliary light AF
As described in the mode flow, # 232 or # 2 in Fig. 14
36. If # 263 is not in fill AF mode, # 2
Reset the stack pointer at 64 and move to # 265.

The flow from here is to determine whether or not to go to the focus detection for confirming whether the stop position of the lens is within the focusing zone after the focus adjustment driving. First,
Check the DR signal sent from the control microcomputer (MC2) to see if it is single shooting mode or continuous shooting mode. If the DR signal is "0", that is, the single shooting mode, # 267
s Wait, the lens will come to a complete stop from low speed, then enter the next focus detection loop. Then, if it is confirmed by the next focus detection that it is within the focusing zone, that is, if it is checked in step # 116 of the main flow of FIG. do. If the position where the lens stops is not within the focusing zone,
The routine for driving the lens is entered again from # 120 in FIG. 11, and the same operation is repeated. This is the flow when confirming the focus. Next, in the continuous shooting mode, since the DR signal is "1", the process proceeds from # 265 to # 266 in FIG. Here, when the lens is stopped (when the driving flag is "0"), the defocus amount (FE
Check RM). If this value is 500 μm or more, proceed to # 267. That is, in the continuous shooting mode, if the defocus amount before driving the lens is 500 μm or more, the focus is confirmed. # 266, FERM is 500μm
If less, go to # 268 and check if the reversal flag is on.If the reversal flag is on, it means that the backlash has been corrected. Go towards. If the reversal flag is not set at # 268, the flow goes to the focus display flow of "INFZ" at # 117. This is a method for increasing the lens drive speed to improve the followability to a moving subject in the continuous shooting mode. When automatic focus adjustment without backlash correction is performed from a position within 500 μm, , The linearity of the system is good, and it goes directly to the in-focus display without performing the focus detection of the in-focus confirmation with the belief that it will surely enter the in-focus zone. In other cases, go to the focus confirmation and improve the focus accuracy. However, if the focus detection capability is further improved and there is almost no drive system error, the focus confirmation may not be necessary here. The above is the sequence of automatic focus adjustment.

Next, "convolution integration" and movement amount correction will be described using the flow from # 40 to # 53 in FIG. 9 and the time charts in FIGS. 18 (A) and (B). This is basically a means for shortening the time required for the focus detection loop. FIG. 18 (A) shows the case where the subject is relatively bright and the integration time of the CCD image sensor (FLM) is less than 60 ms, and FIG. 18 (B) shows the case where the integration time is darker than 60 ms. Then, FIG. 18 (B) is in a state called "convolution integration".

First, when the subject is bright, the value EVTCNT of the event counter when the integration of the sensor is started is read as shown in FIG. 18 (A), and this is saved as T1. At the end of integration
Save T2. Then, immediately after inputting the AGC data, the next integration is started. Assuming that the time when this integration starts is almost the same time as, consider T1 ′ = T2,
T1 'will not be imported again. At the same time when the integration is started, the pixel data is taken in from the CCD image sensor. Then, the focus detection calculation is started. However, in the case of the bright subject (A), the second integration started from has ended by the time the focus detection calculation ends. Pixel data from the CCD image sensor is output immediately after the completion of integration, and the data cannot be held in the sensor until the end of calculation. AF microcomputer (MC
If 1) takes in new data, the data currently being calculated will be destroyed. Eventually, this second integrated data will be discarded. However, if the next integration is started immediately after the calculation ends, the integration time itself does not matter so long as it is bright, and the focus detection loop time does not become long. In this case, the count value in
T2 'will be ignored. The calculation of the movement correction at this time is based on the above-described calculation formula. That is, Tx =
The correction amount Tz = Tx / 2 + Ty when T1-T2 and Ty = T2-T3 may be subtracted from the lens drive count value DRCNT obtained from the calculation result. Here, T3 is the event count value at the end of the calculation. The value DRCNT corrected by is set as the count value EVTCNT of the new event counter. At the start of the next integration, this count value is saved as T1 ″, and so on.

Next, when the subject is dark, the event count value T1 at the start of integration is stored. Ends integration and saves T2. The next integration starts immediately after the AGC data is acquired. Focus detection calculation starts after CCD data is input. Then, the calculation is completed, T3 is obtained, and the movement amount is corrected in the same manner as in (A). At the time when this integration is completed, the second integration is not completed. If the "convolutional integration" method is not used here, a new integration is started at, and a time equivalent to the interval between-is required. However, in this embodiment, "convolution integral" is used.
Since the integration is started immediately by, you only have to wait -21 seconds until the integration is completed. That is, the total time-is shortened. That is,
The “convolution integration” method is effective when the integration time exceeds −time. In this example, − is 60
The maximum integration time of ms or-is 100 ms.

By the way, in the case of (B), the same method as in (A) cannot be applied to the movement correction. The movement correction at the end of calculation 24 is performed by counting the count value T1 'at the start of integration (this is regarded as the count value at the end of the previous integration and can be replaced with T2 → T1') and at the end of integration T2 '. , I want to obtain the correction value using T3 'at the end of calculation, but the lens drive event count value EVTCNT has been rewritten at the end of the previous calculation, that is, when Tx = T1'-T2' in the correction calculation. ,
Since T1 'and T2' are numerical values in different dimensions, this calculation is meaningless. T2 'and T3' are at a new scale from the time when the operation result is obtained and EVTCNT is set. Therefore, T1 'also needs to be converted to the new scale. That is, the drive count value DRCNT obtained in
The difference from the value T3 that came to in the previous scale is the conversion correction amount to the new scale. If the system is ideal, DR
CNT should be T3, but the fact that the lens is moving with respect to the subject is performing sensor integration, and the coefficient between the defocus amount and the lens drive count value is quantized to a smaller value. That is, the defocus amount obtained by the focus detection calculation itself does not include the error due to backlash correction performed when returning too much so that the result is obtained a little smaller to prevent overshooting of the lens. Be sure to consider the DRCN
T> T3. Therefore, DRCNT-T3 becomes the amount of correction between the new scale and the old scale, and when T2 is replaced with T1 ', if this is corrected, T1' of the new scale can be obtained and the movement correction at 24 can be performed. In the embodiment shown in the flow chart, the correction amount Tz is obtained by replacing (DRCNT-T3) + T2 → T1 'with Tx = T1'-T2'. However, if this is another embodiment and Tx = (T2-T3) + (DRCNT-T2 '), the correction amount Tz can be similarly obtained. However, in this case, the correction of (DRCNT-T3) is not required, but another routine for renormalization integration is created at the time of moving amount correction, and the above formula is not prepared instead of Tx = T1'-T2 '. It does not become. Again T
It is also necessary to prepare another memory so that T'is not erased by 2 '.

Next, looking at "convolution integral" on the flowchart,
It starts from # 66 in Figure 10. When it is determined that the lens is being driven by checking the driving flag in # 65, it may or may not be in the “convolution integration” state, but the next integration is started in # 66, and the convolution integration flag ( The renormalization integral F) in Table 5-1 is established. The top of the focus detection loop when "convolution integration" is required is "CDINT" of # 40 in FIG.

Now, follow the flow when it is assumed that the state is that shown in FIG. 18 (B). The integration mode is set in # 40 so that the integration end signal NB4 can be detected. Then, in # 42, it is checked whether or not the renormalization integration flag is set. If not, the renormalization integration mode is not set, so the flow proceeds to # 44.
If the renormalization integration flag is set, the process proceeds to step # 43, where the integration end signal NB4 is checked to see if the integration has already been completed. If the integration is not completed as shown in FIG. 18 (B), the process proceeds to “TINTC” in # 49, that is, the flow from “TINTC” in the renormalization state, # 44
"CDINTS" from is for non-renormalization. # 49 in Figure 10
Then set the 1-cut shot flag to "1". The AFE signal is set to "Low" at # 50, and T1 'is corrected in preparation for movement correction at # 51 as described above. Set the maximum remaining integration time of 40 ms in # 53 and proceed to # 55. The following is the flow of the main routine. The "convolution integration" has the effect of shortening the focus detection time in this way. This concludes the description of the flow of the AF microcomputer (MC1).

EFFECTS OF THE INVENTION According to the present invention, when it is determined that the defocus amount is not equal to or less than the predetermined value, it is determined that the focus is confirmed by the focus confirmation means, and the defocus amount is equal to or less than the predetermined value. If it is determined that the focus is determined to be in focus when the drive of the drive unit by the drive control unit is terminated without operating the focus confirmation unit.

That is, when the driving of the driving unit is completed, the focusing confirmation is performed only when the focusing accuracy is low, and the focusing confirmation is not performed when the focusing accuracy is high.

Therefore, when the focusing accuracy is high, that is, when the DF amount is smaller than the predetermined value, the time required for the focus adjustment becomes shorter than that of the conventional focus adjustment device that always performs the focus confirmation, and the chance of missing a shutter is reduced. To do.

[Brief description of drawings]

FIG. 1 is a schematic diagram showing an entire camera system of an embodiment of the present invention, FIG. 2 is a block diagram showing its electric circuit, and FIG. 3 is a circuit diagram showing a flash circuit of its electronic flash device.
Figure 5 is a flow chart showing the operation of the control microcomputer.
FIG. 6 is a block diagram showing the interface circuit,
FIG. 7-16 is a flow chart showing the operation of the AF microcomputer, FIGS. 17 (A) and (B) are time charts showing the interrupt signal, and FIGS. 18 (A) and (B) are the operations of "convolution integration". FIG. 19 is a time chart for explaining, and FIG. 19 is a schematic diagram for explaining the focus detection principle of the embodiment of the present invention. (113) (MC1); computing means, defocus determination means, inversion determination means, control means, (114) (MDR1) (MO1); drive means.

Claims (3)

[Claims] 1. A focus detection means for calculating a defocus amount of a photographing lens, a driving means for driving a photographing lens, and a driving amount calculation means capable of calculating a driving amount of the driving means from the defocus amount. When the defocus amount exceeds the predetermined focusing width, the driving means is driven based on the calculated driving amount to drive the photographing lens to the in-focus position, while the defocus amount is the predetermined amount. When the focus width is not exceeded, the drive means is stopped and the photographing lens is not driven, and the focus detection means is operated again after the drive control means has finished driving the drive means. Focusing confirmation means for confirming whether or not focus is achieved based on the detection result, determination means for determining whether or not the defocus amount is less than or equal to a predetermined deviation amount, and the defocus amount is predetermined When it is determined that the amount is not less than or equal to the predetermined amount, the first focus determination unit that confirms by the focus confirmation unit after the drive control unit finishes driving the drive unit, and the defocus amount is less than or equal to a predetermined shift amount. If it is determined that the second focus determination means determines that the focus is in focus, the drive control means does not perform confirmation by the focus confirmation means after the drive of the drive means is finished. Automatic focus adjustment device. 2. The automatic focusing apparatus according to claim 1, wherein the first and second focusing determination means have a display means for displaying that focusing is achieved when it is determined that focusing is achieved. Focus adjustment device. 3. The first and second in-focus determination means include inhibition means for inhibiting the operation of the exposure control means of the camera until it is determined that the in-focus state is achieved. An automatic focusing device according to the item.