Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JPS6233999B2 - - Google Patents
[go: Go Back, main page]

JPS6233999B2 - - Google Patents

Info

Publication number
JPS6233999B2
JPS6233999B2 JP54161868A JP16186879A JPS6233999B2 JP S6233999 B2 JPS6233999 B2 JP S6233999B2 JP 54161868 A JP54161868 A JP 54161868A JP 16186879 A JP16186879 A JP 16186879A JP S6233999 B2 JPS6233999 B2 JP S6233999B2
Authority
JP
Japan
Prior art keywords
ship
output
calculating
subtraction
heading
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
JP54161868A
Other languages
Japanese (ja)
Other versions
JPS5686894A (en
Inventor
Chogo Sekine
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Japan Radio Co Ltd
Original Assignee
Japan Radio Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Japan Radio Co Ltd filed Critical Japan Radio Co Ltd
Priority to JP16186879A priority Critical patent/JPS5686894A/en
Publication of JPS5686894A publication Critical patent/JPS5686894A/en
Publication of JPS6233999B2 publication Critical patent/JPS6233999B2/ja
Granted legal-status Critical Current

Links

Landscapes

  • Navigation (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Description

【発明の詳細な説明】 本発明は船舶を予定の航路上を逸脱せずに目的
地迄誘導するオートパイロツト装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an autopilot device for guiding a ship to a destination without deviating from a planned route.

第1図は従来のオートパイロツト装置の構成を
示す。図において、1はジヤイロ信号の入力端
子、2は針路設定器、3は引算器、4はPID
(proportional、integrate、differential)演算制
御器である。次にこの動作を説明する。ジヤイロ
信号入力端子1に伝えられるジヤイロ信号即ち船
首方位信号と針路設定器2に手動で設定された船
が航行しようとする方位は引算器3で差が演算さ
れ演算結果はPID演算制御器4に送給される。
PID演算器4は一般に第1式の演算を行う。
FIG. 1 shows the configuration of a conventional autopilot device. In the figure, 1 is the input terminal for the gyro signal, 2 is the course setter, 3 is the subtracter, and 4 is the PID.
(proportional, integral, differential) calculation controller. Next, this operation will be explained. The difference between the gyro signal, that is, the heading signal, transmitted to the gyro signal input terminal 1 and the direction in which the ship is sailing, which is manually set in the course setting device 2, is calculated by a subtractor 3, and the calculation result is sent to a PID calculation controller 4. will be sent to
The PID calculator 4 generally performs the calculation of the first equation.

y=VPx+VI∫xdt+VDdx/dt ……(1) ここでyはPID演算制御器の出力、 xはPID演算制御器の入力、 tは時間 VP、VI、VDはそれぞれ比例(P)、積
分(I)、微分(D)の演算の係数 PID演算制御器4の出力は舵取機5に送給さ
れ、舵取機5により舵6が動かされ船は向きを変
えて船首方位が常に設定方位と等しくなるように
制御される。即ち保針制御が行なわれる。
y = VP _ _ _ Coefficients for proportional (P), integral (I), and differential (D) calculations The output of the PID calculation controller 4 is sent to the steering gear 5, which moves the rudder 6 and changes the direction of the ship. The heading is controlled so that the heading is always equal to the set heading. That is, course keeping control is performed.

第2図は第1図のオートパイロツト装置を使用
して船が現在位置P1から目的地P2に向つて航行す
る場合の説明図である。
FIG. 2 is an explanatory diagram of a case where a ship navigates from a current position P1 to a destination P2 using the autopilot device shown in FIG.

現在位置P1から目的地P2を望む方位即ち目的地
方位がθであつたとすると航海士は針路設定器2
にθを設定する。このとき第1図のオートパイロ
ツト装置は船首方位が常にθとなるように舵取機
5に出力を与え舵6を動かすが、潮流、海流、
風、浪などの外力Fが船に加わると、船は外力F
の向きに流される。従つて船首方位は設定針路θ
を保ちながらもP1,P2を結ぶ線上から遠ざかり第
2図P3で示すような地点を航行するようになつて
しまう不都合が有つた。そのため航海士は目的地
P2に首尾良く到達するために外力Fを推定して、
その影響を相殺する分だけ補正して設定針路を設
定していたが、外力Fの大きさは時々刻々変化す
るものでありまた外力Fの適当な測定手段が無い
ので通常目的地P2に良い精度で到達する事は困難
であつた。
If the direction from the current position P 1 to the destination P 2 , that is, the destination position is θ, the navigator should use the course setting device 2.
Set θ to . At this time, the autopilot device shown in Fig. 1 applies an output to the steering gear 5 to move the rudder 6 so that the ship's heading is always at θ, but the tidal current, ocean current,
When an external force F such as wind or waves is applied to a ship, the ship will be affected by the external force F.
be swept away in the direction of Therefore, the heading is the set course θ
However, the problem was that the ship moved away from the line connecting P 1 and P 2 and ended up sailing to a point as shown in Figure 2, P 3 . Therefore, the navigator is the destination
Estimate the external force F to successfully reach P 2 ,
The set course was set by making a correction to offset the influence, but since the magnitude of the external force F changes from moment to moment, and there is no suitable means of measuring the external force F, it is usually better to set the course for destination P2 . It was difficult to achieve this with precision.

また、従来、船舶を予定の航路に沿つて目的地
まで誘導するオートパイロツトとして、設定針路
と位置測定器で測定した過去の実進路方位との誤
差を求め、この誤差を補償したものを新たな航行
方位とするものや、船舶の現在位置から目的地を
望む方位を算出し、その方位を設定針路として自
動的に設定するもの等が知られていたが、これら
はいずれも針路修正のための情報を求めるのに、
自動航行開始点の位置と目的地の位置とを結ぶ予
定の航路のデータを使用していないので、船舶が
潮流、海流、風、浪などの外力を受けて予定の航
路から逸脱し易く、また、一度逸脱した場合に
は、予定の航路に復帰する能力に欠ける等の欠点
があつた。
In addition, conventional autopilots have been used to guide ships along a planned route to their destination by determining the error between the set course and the past actual course direction measured by a position measuring device, and then creating a new version that compensates for this error. There are some methods that use the navigation direction as a navigation direction, and others that calculate the desired direction of the destination from the ship's current position and automatically set that direction as the set course, but these are all methods for course correction. When asking for information,
Since the data of the planned route connecting the automatic navigation start point position and the destination position is not used, it is easy for the ship to deviate from the planned route due to external forces such as tides, ocean currents, wind, and waves. However, there were drawbacks such as the inability to return to the planned route once the vessel deviated.

従来装置のこうした欠点は測量船や資源探査船
などのように調査海域を基盤の目のように規則正
しく分割した予定の航路上を極力精密に船を航行
させる目的には大きな障害となつていた。
These shortcomings of conventional equipment have been a major hindrance to the purpose of allowing ships, such as survey vessels and resource exploration vessels, to navigate as precisely as possible along scheduled routes that divide the survey area into regular sections like the eyes of a base.

本発明はこれらの欠点を除去するため、オート
パイロツト装置への入力として単にジヤイロコン
パスなどにより測定される船首方位信号ばかりで
なくロランC受信機などの位置測定装置により測
定した自船の位置情報も同時に使用し、船が予定
の航路上を逸脱することなく航行するようにした
もので以下図面により詳細に説明する。
In order to eliminate these drawbacks, the present invention uses not only the heading signal measured by a gyro compass as input to the autopilot system, but also the own ship's position information measured by a position measuring device such as a Loran C receiver. It is also used at the same time to ensure that the ship sails without deviating from the planned route, and will be explained in detail below with reference to the drawings.

第3図は本発明の一実施例であり、第4図はそ
の動作説明図である。第3図において、7はロラ
ンC受信機などの位置測定装置により測定された
自船位置の入力端子、8は自動航行開始点記憶
器、9は自動航行開始スイツチ、10は航行方位
距離演算器、11は第1の引算器、12は目的地
方位設定器、13は正弦演算器、14は掛算器、
15は第1のPID演算器、16は第2の引算器、
以下1はジヤイロコンパス方位入力端子、3は第
3の引算器、4は第2のPID演算器で第1図と同
一構成である。
FIG. 3 shows an embodiment of the present invention, and FIG. 4 is an explanatory diagram of its operation. In Fig. 3, 7 is an input terminal for own ship's position measured by a position measuring device such as a Loran C receiver, 8 is an automatic navigation start point memory, 9 is an automatic navigation start switch, and 10 is a navigation direction and distance calculator. , 11 is a first subtractor, 12 is a destination position setter, 13 is a sine operator, 14 is a multiplier,
15 is the first PID calculator, 16 is the second subtractor,
Hereinafter, 1 is a gyro compass azimuth input terminal, 3 is a third subtractor, and 4 is a second PID calculator, which has the same configuration as in FIG. 1.

次にこの動作を両図を用いて説明する。端子7
にはロランC受信機などにより測定した自船の位
置データが伝えられる。第4図P1の地点で自動航
行開始スイツチ9をa側に倒すと、接点c→aの
経路で接地信号が自動航行開始点記憶器8の1方
の入力端子に伝えられる。この時自動航行開始点
記憶器8は他方の入力端子に端子7より伝えられ
る自船の位置データP1を記憶する。記憶されたデ
ータP1は自動航行開始スイツチ9がa側に投入さ
れている間持続する。次に船が第4図P3の地点迄
航行した時の本装置の動作を説明する。航行方位
距離演算器10は1方の入力端子に自動航行開始
点記憶器8の出力端子から伝えられる自動航行開
始時の自船位置データP1と他方の入力端子に端子
7から伝えられる自船の現在位置データP3とを用
いて、自船が自動航行開始点P1に対する現在位置
P3の方位及び距離、すなわちそれぞれ第4図のα
及び線分1 3を演算し、方位は第1の引算器11
に、距離は掛算器14に伝達する。目的地方位設
定器12には第4図に示すように船が現在位置か
らP3から目的地P2を望む方位θが航海士の手によ
り設定される。第1の引算器11は航行方位距離
演算器10から伝えられる自船の航行方位αから
目的地方位設定器12に設定された目的地方位θ
を引きその結果即ち第4図のβを正弦演算器13
に伝達する。正弦演算器13の出力はsinβであ
り掛算器14の1方の入力端子に伝えられる。掛
算器14の他方の入力端子には航行方位距離演算
器10の1方の出力である第4図のP1からP3迄の
距離1 3が伝えられ掛算器14では1 3sinβが
演算され出力としてPID演算器15に伝達され
る。1 3sinβは点P3からP1,P2を結ぶ予定の航
路におろした垂線の距離即ち点P3の予定の航路か
らの隔りを示す。次に掛算器14の出力を入力と
するPID演算器15は第1式と同様な演算を行な
うが演算結果は目的地方位設定器12に設定した
目的地方位βと船の航行方位との差βを取除くた
めに修正すべき船首方位であり、これは第4図に
示すγである。なおPID演算器15は自動航行開
始スイツチ9の接点bが結ばれ、自動航行開始ス
イツチ9がb側に倒されている間はすべての演算
が停止させられ出力が零にさせられるが、自動航
行開始スイツチ9がa側に倒されたときからPID
演算を開始し出力γを第2の引算器16の1方の
入力端子に伝える。さらに第2の引算器16は目
的地方位設定器12に設定された目的地方位θと
PID演算器15の出力である修正すべき船首方位
γとの差を算出する。この差は予定の航路に戻る
ために向けるべき船首方位を示しているのでこれ
を第1図の針路設定器2の出力の代りとして第1
図と同様の第3の引算器3に送給し、以下第1図
のオートパイロツト装置のそれ以外の部分は従来
装置と全く同様に動作させればこの差、即ち予定
の航路に戻るために向けるべき船首方位の方向に
実際に船首が向くように舵が切られる。
Next, this operation will be explained using both figures. terminal 7
The ship's position data measured by the Loran-C receiver is transmitted to the ship. When the automatic navigation start switch 9 is turned to the a side at the point P1 in FIG. 4, a grounding signal is transmitted to one input terminal of the automatic navigation start point memory 8 via the path from contact point c to a. At this time, the automatic navigation start point memory 8 stores the own ship's position data P 1 transmitted from the terminal 7 to the other input terminal. The stored data P1 persists while the automatic navigation start switch 9 is turned to the a side. Next, the operation of this device when the ship has sailed to the point P3 in Figure 4 will be explained. The navigation direction and distance calculator 10 has one input terminal containing own ship position data P 1 transmitted from the output terminal of the automatic navigation start point memory 8 at the time of automatic navigation start, and the other input terminal the own ship position data P 1 transmitted from the terminal 7. Using current position data P3 , own ship's current position with respect to automatic navigation starting point P1
The direction and distance of P 3 , i.e. α in Fig. 4, respectively.
and line segment 1 3 , and the direction is calculated by the first subtractor 11
Then, the distance is transmitted to multiplier 14. As shown in FIG. 4, the destination position setting device 12 is set by the navigator's hand as the direction θ in which the ship desires to view the destination P 2 from the current position P 3 . A first subtractor 11 calculates the destination position θ set in the destination position setting device 12 from the own ship's navigation direction α transmitted from the navigation direction and distance calculator 10.
The result, ie, β in FIG. 4, is calculated by the sine operator 13
to communicate. The output of the sine calculator 13 is sin β and is transmitted to one input terminal of the multiplier 14. The other input terminal of the multiplier 14 is transmitted with the distance 1 3 from P 1 to P 3 in FIG . It is transmitted to the PID calculator 15 as an output. 1 3 sinβ indicates the distance of a perpendicular line drawn from point P 3 to the planned route connecting P 1 and P 2 , that is, the distance of point P 3 from the planned route. Next, the PID calculator 15 which receives the output of the multiplier 14 as input performs a calculation similar to the first equation, but the calculation result is the difference between the destination position β set in the destination position setting device 12 and the ship's navigation direction. This is the heading that should be corrected to remove β, which is γ shown in FIG. Note that the PID calculator 15 is connected to the contact point b of the automatic navigation start switch 9, and while the automatic navigation start switch 9 is pushed to the b side, all calculations are stopped and the output is made zero, but automatic navigation is not possible. PID from when start switch 9 is turned to side a
The calculation is started and the output γ is transmitted to one input terminal of the second subtracter 16. Furthermore, the second subtractor 16 is connected to the destination position θ set in the destination position setter 12.
The difference between the heading γ, which is the output of the PID calculator 15, and the heading γ to be corrected is calculated. Since this difference indicates the heading direction that the ship should face in order to return to the planned course, this difference is used as the first heading in place of the output of the course setting device 2 shown in
If the feed is sent to the third subtractor 3 similar to the one shown in the figure, and the other parts of the autopilot device shown in FIG. The rudder is turned so that the bow actually points in the direction that the ship should be heading.

なお正弦演算器13を省略し、第2の引算器1
6を第3の引算器3と合せて構成しても等価な装
置が実現出来る。
Note that the sine calculator 13 is omitted, and the second subtracter 1
6 and a third subtractor 3, an equivalent device can be realized.

以上説明したように本発明によれば、船首方位
の修正が予定の航路と船舶の現在位置との隔りに
基いて行なわれ、この隔りが取除かれるように自
動制御される結果、航海士が設定した針路と船の
航行方位が常に一致するように自動制御されるの
で、航海士は従来装置と全く同様の針路設定操作
を行うにも拘らず船は外力に抗して予定の航路上
を航行出来る利点があり、調査船、漁船などの精
密自動操船が可能になる。
As explained above, according to the present invention, the ship's heading is corrected based on the gap between the planned route and the current position of the ship, and as a result of automatic control to remove this gap, the navigation Since the ship is automatically controlled so that the course set by the navigator always matches the ship's heading, the ship resists external forces and follows the planned course even though the navigator performs the same course setting operations as with conventional systems. It has the advantage of being able to navigate above the surface, making it possible to conduct precise automatic maneuvering of research vessels, fishing boats, etc.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は従来のオートパイロツトの構成を示す
説明図、第2図は従来のオートパイロツトの動作
を説明する説明図、第3図は本発明装置の構成を
示す説明図、第4図は本発明装置の動作を説明す
る説明図である。 3,11,16…引算器、4,15…PID演算
器、5…舵取機、6…舵、7…自船の位置データ
の入力端子、8…自動航行開始記憶器、9…自動
航行開始スイツチ、10…航行方位距離演算器、
12…目的地方位設定器、13…正弦演算器、1
4…掛算器。
FIG. 1 is an explanatory diagram showing the configuration of a conventional autopilot, FIG. 2 is an explanatory diagram explaining the operation of a conventional autopilot, FIG. 3 is an explanatory diagram showing the configuration of the device of the present invention, and FIG. FIG. 3 is an explanatory diagram illustrating the operation of the invention device. 3, 11, 16... Subtractor, 4, 15... PID calculator, 5... Steering gear, 6... Rudder, 7... Own ship position data input terminal, 8... Automatic navigation start memory, 9... Automatic Navigation start switch, 10... Navigation direction and distance calculator,
12... Destination position setter, 13... Sine calculator, 1
4... Multiplier.

Claims (1)

【特許請求の範囲】[Claims] 1 船舶用オートパイロツト装置において、自動
航行開始スイツチと船位データの入力端子と、目
的地方位の設定手段と、自動航行開始点の位置デ
ータを記憶する手段と、自動航行開始点の位置デ
ータと現在位置データとから航行方位及び距離を
算出する手段と、該航行方位と目的地方位の差を
演算する第1の引算手段と、該第1の引算手段の
出力の正弦を求める演算手段と、該演算手段の出
力と航行距離の積を求める掛算手段と、該掛算手
段の出力をPID演算する第1のPID演算手段と、
該PID演算手段の出力と目的地方位の差を演算す
る第2の引算手段と、船首方位信号の入力端子
と、該船首方位と第2の引算手段出力との差を求
める第3の引算手段と、該第3の引算段出力を
PID演算し舵取器を制御する第2のPID演算制御
手段とを有することを特徴とした船舶用オートパ
イロツト装置。
1 In a marine autopilot device, an automatic navigation start switch, an input terminal for ship position data, a means for setting the destination position, a means for storing position data of the automatic navigation start point, a means for storing the position data of the automatic navigation start point and the current position data. means for calculating the navigation direction and distance from the position data; first subtraction means for calculating the difference between the navigation direction and the destination position; and calculation means for calculating the sine of the output of the first subtraction means. , a multiplication means for calculating the product of the output of the calculation means and the cruising distance, and a first PID calculation means for performing a PID calculation on the output of the multiplication means;
a second subtraction means for calculating the difference between the output of the PID calculation means and the destination position, an input terminal for a heading signal, and a third subtraction means for calculating the difference between the heading and the output of the second subtraction means. a subtraction means and the output of the third subtraction stage;
A marine autopilot device comprising: second PID calculation control means for calculating PID and controlling a steering gear.
JP16186879A 1979-12-13 1979-12-13 Marine autopilot device Granted JPS5686894A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP16186879A JPS5686894A (en) 1979-12-13 1979-12-13 Marine autopilot device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP16186879A JPS5686894A (en) 1979-12-13 1979-12-13 Marine autopilot device

Publications (2)

Publication Number Publication Date
JPS5686894A JPS5686894A (en) 1981-07-15
JPS6233999B2 true JPS6233999B2 (en) 1987-07-23

Family

ID=15743482

Family Applications (1)

Application Number Title Priority Date Filing Date
JP16186879A Granted JPS5686894A (en) 1979-12-13 1979-12-13 Marine autopilot device

Country Status (1)

Country Link
JP (1) JPS5686894A (en)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5563997A (en) * 1978-11-06 1980-05-14 Yokogawa Hokushin Electric Corp Automatic navigation equipment

Also Published As

Publication number Publication date
JPS5686894A (en) 1981-07-15

Similar Documents

Publication Publication Date Title
JP7417538B2 (en) Control target generation device and ship maneuvering control device
US11597488B2 (en) Ship maneuvering system, ship, and ship maneuvering method
JP2017154734A (en) Improved marine vessel maneuvering methods and systems
JP3949932B2 (en) Autonomous underwater vehicle navigation control system
EP4389589B1 (en) Steering system having function of correcting steering angle of uniaxial two-rudder vessel
CN113126492B (en) Automatic path tracking method for dynamic positioning ship
JPH0133398B2 (en)
Xinjing et al. Horizontal path following for underactuated AUV based on dynamic circle guidance
JP4804032B2 (en) Automatic navigation assistance system for ships
JPS6234000B2 (en)
JPS6233998B2 (en)
US3576977A (en) System and method for controlling the positioning system of a pipelaying vessel
US4238824A (en) Line length navigation system
JPS6233999B2 (en)
Ohtsu et al. A fully automatic berthing test using the training ship Shioji Maru
JPH0578476B2 (en)
JPH0633076B2 (en) Auto pilot device
JPH0120643Y2 (en)
JPH0414287B2 (en)
JPH0213324B2 (en)
JPS61232993A (en) Automatic navigating device
US20250321594A1 (en) Systems and methods for controlling a watercraft via propulsion devices
JPH04255Y2 (en)
JPH04133897A (en) Ship maneuvering assisting device
JPS5926518B2 (en) Marine automatic steering system