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JPS6364726B2 - - Google Patents
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JPS6364726B2 - - Google Patents

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Publication number
JPS6364726B2
JPS6364726B2 JP57027750A JP2775082A JPS6364726B2 JP S6364726 B2 JPS6364726 B2 JP S6364726B2 JP 57027750 A JP57027750 A JP 57027750A JP 2775082 A JP2775082 A JP 2775082A JP S6364726 B2 JPS6364726 B2 JP S6364726B2
Authority
JP
Japan
Prior art keywords
value
movement
positioning
amount
navigation device
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
JP57027750A
Other languages
Japanese (ja)
Other versions
JPS58216910A (en
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 filed Critical
Priority to JP57027750A priority Critical patent/JPS58216910A/en
Publication of JPS58216910A publication Critical patent/JPS58216910A/en
Publication of JPS6364726B2 publication Critical patent/JPS6364726B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S5/00Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/02Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves

Landscapes

  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Navigation (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)

Description

【発明の詳細な説明】 この発明はロラン、オメガ、デツカ等の電波航
法装置を用いた測位方法に関し、特には電波航法
特有の誤差要因に基づく影響を少なくして航法装
置の見かけ上の測位精度を向上する方法に関す
る。
[Detailed Description of the Invention] The present invention relates to a positioning method using radio navigation devices such as Loran, Omega, Detsuka, etc., and in particular, the apparent positioning accuracy of the navigation device by reducing the influence of error factors specific to radio navigation. on how to improve.

電波航法特有の誤差要因として位置線の発散と
交角があるが、この影響は発散が大きく且つ交角
が小さくなるにしたがつて大きくなる。たとえ
ば、時間差0.1μs単位で位置線を求めるロランで
は、ベースライン同志の交点付近等においては誤
差が40〜50m程度と比較的小さいが、発散と交角
の最も悪い状態の位置においては誤差が200〜300
mにおよぶ。つまり海域によつては、0.1μsの変
動で、表示される緯度経度に200〜300mの位置の
ずれが発生することになる。そこでこの誤差を無
くし精度を向上する目的で、従来は適宜測位デー
タの平均処理をおこなう測位方法を実施してい
た。この方法は、測位データを適当な期間内で指
数平滑等によつて平均処理し、その結果を現在の
測位位置とする方法である。
Error factors specific to radio navigation include the divergence and intersection angle of position lines, and this influence increases as the divergence increases and the intersection angle decreases. For example, in Loran, which calculates position lines with a time difference of 0.1 μs, the error is relatively small at around 40 to 50 m near the intersection of baselines, but at the position where the divergence and intersection angle are the worst, the error is 200 to 50 m. 300
It extends to m. In other words, depending on the sea area, a change of 0.1 μs will cause a positional shift of 200 to 300 meters in the displayed latitude and longitude. Therefore, in order to eliminate this error and improve accuracy, conventionally a positioning method has been implemented in which positioning data is averaged as appropriate. In this method, positioning data is averaged by exponential smoothing or the like within an appropriate period, and the result is used as the current positioning position.

しかしながら、このような測位方法は平均処理
のために時間遅れが生じ、しかも精度をより向上
しようとすればその分さらに時間遅れが生じる欠
点があつた。
However, such a positioning method has the disadvantage that a time delay occurs due to averaging processing, and furthermore, if the accuracy is to be further improved, a further time delay occurs.

この発明の目的は、時間遅れを生じることがな
く、しかも位置線の発散が大きく且つ交角の小さ
い海域においても誤差が大きくならない測位方法
を提供することにある。
An object of the present invention is to provide a positioning method that does not cause time delays and does not cause large errors even in sea areas where position lines have a large divergence and a small intersection angle.

この発明は200〜300mにおよぶ誤差は、それを
速度に換算した場合に通常起こり得る船速の範囲
を大きく越えるという点に着目してなされたもの
である。
This invention was made based on the fact that an error of 200 to 300 m greatly exceeds the normal ship speed range when converted into speed.

この発明は電波航法と推測航法とを組合わせた
ハイブリツド航法において、推測航法装置の速度
情報に基いて船の移動量制限幅を設定し、電波航
法機器の測位結果に基く移動量測定値を前記制限
幅と比較し、該測定値が制限幅内にあるときはそ
のままの値を、最大値を越えるときは最大値を、
最小値以下のときは最小値をもつて移動量と見做
すことを特徴とする。
In hybrid navigation that combines radio navigation and dead reckoning, this invention sets a movement limit range for a ship based on speed information from a dead reckoning device, and calculates the measured movement value based on the positioning result of the radio navigation device. Compare with the limit width, if the measured value is within the limit width, use the same value, if it exceeds the maximum value, change the maximum value,
The feature is that when the amount is less than the minimum value, the minimum value is regarded as the amount of movement.

以下この発明の実施例を図面を参照して説明す
る。
Embodiments of the present invention will be described below with reference to the drawings.

第1図はこの発明の測位方法を実施する航法装
置のブロツク図、第2図は同航法装置の動作を示
すフローチヤートである。
FIG. 1 is a block diagram of a navigation device that implements the positioning method of the present invention, and FIG. 2 is a flowchart showing the operation of the navigation device.

この実施例の航法装置は、電波航法と推定航法
とを組合わせたハイブリツド航法を用い電波航法
機器としてロラン1を用い、船の移動量の制限幅
を設定するためにログおよびジヤイロコンパスを
含む推測航法機器2を用いている。
The navigation device of this embodiment uses hybrid navigation that combines radio navigation and dead-reckoning navigation, uses Loran 1 as the radio navigation device, and includes a log and a gyroscope to set limits on the amount of movement of the ship. Dead reckoning navigation equipment 2 is used.

ロラン1は位置線1(以下lop1という)、位置
線2(以下lop2という)および局コードを出力
し、緯度・経度変換部3がこれらの情報から緯
度・経度情報を算出する。算出された緯度・経度
情報は表示器4に表示される。
Loran 1 outputs position line 1 (hereinafter referred to as lop1), position line 2 (hereinafter referred to as lop2), and station code, and latitude/longitude converter 3 calculates latitude/longitude information from these information. The calculated latitude and longitude information is displayed on the display 4.

推測航法機器2は船速を緯度方向の速度Vと
経度方向の速度Vλに分けて出力し、位置変化量
演算部5はこの速度情報から基準位置に対するロ
ランのlop測定時間毎の位置変化量の制限幅Dを、
緯度方向の制限幅D1と経度方向の制限幅D2とし
て算出して緯度・経度変換部3に出力する。
The dead reckoning device 2 outputs the ship speed divided into a speed V in the latitude direction and a speed Vλ in the longitude direction, and the position change calculation unit 5 calculates the position change for each lop measurement time of Loran with respect to the reference position from this speed information. The limit width D is
The limit width D 1 in the latitude direction and the limit width D 2 in the longitude direction are calculated and output to the latitude/longitude converter 3 .

次に第2図を参照してこの航法装置の動作を説
明する。
Next, the operation of this navigation device will be explained with reference to FIG.

第2図Aは推測航法機器2と位置変化量演算部
5からなる推測航法装置の動作手順を示す。ステ
ツプn1(以下ステツプniを単にniという)では推
測航法機器2で緯度方向速度Vと経度方向速度
Vλとが測定される。通常この速度単位はKT(ノ
ツト)である。n2ではこの速度V,Vλに誤差許
容値を加減算して、通常起こり得ると考えられる
速度制限値(最小値および最大値)を求める。こ
の例では上記の誤差許容値を5KTとしているが、
この値は海域等によつて可変するようにしてもい
い。次にn3では上記の速度制限値とロラン1の測
定間隔とから、その測定時間毎の移動量制限値を
求め、その最小値と最大値との差つまり移動最制
限幅Dを求める。dmin、dmaxは緯度方向の
移動量最小(制限)値、移動量最大(制限)値で
あり、dλmin、dλmaxは経度方向の移動量最小
(制限)値、移動量最大(制限)値である。
FIG. 2A shows the operating procedure of the dead reckoning navigation device consisting of the dead reckoning device 2 and the position change calculation unit 5. At step n 1 (hereinafter step ni is simply referred to as ni), the dead reckoning device 2 calculates the latitudinal velocity V and the longitudinal velocity.
Vλ is measured. Usually this speed unit is KT (knots). In n 2 , an error tolerance value is added or subtracted from these speeds V and Vλ to obtain speed limit values (minimum value and maximum value) that are considered to normally occur. In this example, the above error tolerance is 5KT,
This value may be varied depending on the sea area, etc. Next, at n3 , the movement amount limit value for each measurement time is determined from the above-mentioned speed limit value and the measurement interval of Loran 1, and the difference between the minimum value and the maximum value, that is, the maximum movement limit width D is determined. dmin and dmax are the minimum (restriction) value and maximum (restriction) value for the amount of movement in the latitude direction, and dλmin and dλmax are the minimum (restriction) value and maximum (restriction) value for the amount of movement in the longitudinal direction.

一方、以上の動作と非同期に第2図Bに示す動
作がロラン航法装置で実行される。この第2図B
に示す手順はn13とn20を除きすべて緯度・経度変
換部3で実行され、実際には同変換部3に内蔵さ
れているマイクロコンピユータで実行される。
On the other hand, the operation shown in FIG. 2B is executed by the Loran navigation device asynchronously with the above operation. This figure 2B
All of the steps shown in , except for n 13 and n 20 , are executed by the latitude/longitude converter 3, and are actually executed by the microcomputer built in the converter 3.

まずn10では、今から測位しようとする位置の
基準位置となる推測位置q(緯度位置)、λq(経度
位置)が設定される。この推測位置は通常、前回
の測位位置である。n11ではその推測位置と局コ
ードから求めた主従局位置とから、lop変化量を
緯度・経度変化量に換算するための変換係数α,
βを求める。続いてn12で推測位置のlopTC1
TC2を求める。次にn13で現在位置のlopT1,T2
をロラン1で測定する。そしてこの測定lopT1
T2と計算によつて得た推測位置のlopTC1,TC2
の差dT1,dT2をlop変化量として求め(n14)、さ
らにこのlop変化量を上記変換係数α,βを用い
て緯度・経度変化量d,dλにする。
First, in n10 , estimated positions q (latitude position) and λq (longitude position), which are the reference positions of the position to be measured from now on, are set. This estimated position is usually the previously determined position. In n 11 , from the estimated position and the master and slave station positions obtained from the station code, a conversion coefficient α,
Find β. Then the estimated position lopTC 1 at n 12 ,
Find TC 2 . Next, at n 13 , the current position lopT 1 , T 2
is measured with Loran 1. And this measurement lopT 1 ,
T 2 and the estimated position lopTC 1 , TC 2 obtained by calculation
The differences dT 1 and dT 2 are obtained as lop changes (n 14 ), and these lop changes are converted into latitude/longitude changes d and dλ using the conversion coefficients α and β.

このn10〜n15の手順は従来の測位方法の手順と
全く同じである。
This procedure of n 10 to n 15 is exactly the same as the procedure of the conventional positioning method.

n16〜n19は以上の手順で求めた変化量をn3で求
めた制限幅Dに抑制するステツプである。最初に
n16でn3において求めた緯度方向の移動量の制限
幅D1とdとを、また経度方向の移動量の制限幅
D2とdλとをそれぞれ比較する。そしてd,dλと
もに制限幅D1,D2内にあれば、そのd,dλは測
位位置計算をおこなうための値△,△λとする
が(n17)、dまたはdλが制限幅D1またはD2を越
えてていればn18で進む。すなわち、dがdmin
以下であれば△=dminとされ、dがdmax
以上であれば△=dmaxとされる。またdλが
dλmin以下であれば△λ=dλminとされ、dλが
dλmax以上であれば△λ=dλmaxとされる。こ
のようにn18では、ロラン1の測位結果に対して
制限を与え、その測位結果に基づく移動量が通常
考えられる移動量の最大値を越えるときにはその
最大値をそのときの移動量とみなし、また測位結
果に基づく移動量が通常考えられる移動量の最小
値に達しないときにはその最小値をそのときの移
動量とみなしている。
Steps n 16 to n 19 are steps for suppressing the amount of change obtained in the above procedure to the limit width D obtained in step n 3 . At first
In n 16 , the limit width D 1 and d of the amount of movement in the latitude direction obtained in n 3 , and the limit width of the amount of movement in the longitudinal direction
Compare D 2 and dλ respectively. If both d and dλ are within the limit width D 1 and D 2 , then d and dλ are set to the values △ and △λ for positioning position calculation (n 17 ), but if d or dλ is within the limit width D 1 Or if it is over D 2 , proceed with n 18 . That is, d is dmin
If it is less than or equal to △=dmin, and d is dmax
If it is above, Δ=dmax. Also, dλ
If dλmin or less, △λ=dλmin, and dλ is
If it is greater than or equal to dλmax, Δλ=dλmax. In this way, in n 18 , a limit is placed on the positioning result of Loran 1, and when the amount of movement based on the positioning result exceeds the maximum value of the amount of movement that is normally considered, that maximum value is considered as the amount of movement at that time, Further, when the amount of movement based on the positioning result does not reach the minimum value of the amount of movement that is normally considered, the minimum value is regarded as the amount of movement at that time.

こうして移動量△,△λが求められると、こ
の値を元の推測位置q,λqにそれぞれ加算して
測位位置s,λsを求め(n19)、さらにその値を表
示器4に表示して(n20)、次の測位のために推測
位置の更新をおこなう(n21)。以上の処理をロラ
ン1の測定時間毎に実行していく。
Once the movement amounts △ and △λ are obtained in this way, these values are added to the original estimated positions q and λq to obtain the measured positions s and λs (n 19 ), and the values are further displayed on the display 4. (n 20 ), and updates the estimated position for the next positioning (n 21 ). The above processing is executed every measurement time of Loran 1.

以上のようにこの発明によれば、測位位置が位
置線の発散が大きく且つ交角の小さい海域であつ
ても測位位置の変化のバラツキを小さくでき、そ
れ故平均処理をしなくてもすなわち時間遅れのな
い状態で測位誤差を小さくすることができる。
As described above, according to the present invention, even if the positioning position is in a sea area where the position lines have a large divergence and a small intersection angle, it is possible to reduce the variation in the change in the positioning position. positioning error can be reduced without

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

第1図はこの発明の測位方法を実施する航法装
置のブロツク図、第2図は同航法装置の動作を示
すフローチヤートである。
FIG. 1 is a block diagram of a navigation device that implements the positioning method of the present invention, and FIG. 2 is a flowchart showing the operation of the navigation device.

Claims (1)

【特許請求の範囲】[Claims] 1 電波航法と推測航法とを組合わせたハイブリ
ツド航法において、推測航法装置の速度情報に基
いて船の移動量制限幅を設定し、電波航法機器の
測位結果に基く移動量測定値を前記制限幅と比較
し、該測定値が制限幅内にあるときはそのままの
値を、最大値を越えるときは最大値を、最小値以
下のときは最小値をもつて移動量と見做すことを
特徴とする測位方法。
1. In hybrid navigation that combines radio navigation and dead reckoning, a ship's movement limit width is set based on the speed information of a dead reckoning navigation device, and the movement distance measurement value based on the positioning result of the radio navigation device is used as the limit width. When the measured value is within the limit range, the value is taken as is, when it exceeds the maximum value, the maximum value is taken, and when it is below the minimum value, the minimum value is taken as the movement amount. positioning method.
JP57027750A 1982-02-22 1982-02-22 Position measuring method in radio navigation system Granted JPS58216910A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP57027750A JPS58216910A (en) 1982-02-22 1982-02-22 Position measuring method in radio navigation system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP57027750A JPS58216910A (en) 1982-02-22 1982-02-22 Position measuring method in radio navigation system

Publications (2)

Publication Number Publication Date
JPS58216910A JPS58216910A (en) 1983-12-16
JPS6364726B2 true JPS6364726B2 (en) 1988-12-13

Family

ID=12229698

Family Applications (1)

Application Number Title Priority Date Filing Date
JP57027750A Granted JPS58216910A (en) 1982-02-22 1982-02-22 Position measuring method in radio navigation system

Country Status (1)

Country Link
JP (1) JPS58216910A (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102721417B (en) * 2011-12-23 2015-03-25 北京理工大学 Method for restraining coarse alignment error of solidification inertial system of strapdown inertial navigation system
JP7069624B2 (en) * 2017-10-05 2022-05-18 日産自動車株式会社 Position calculation method, vehicle control method and position calculation device
CN109596127A (en) * 2018-12-04 2019-04-09 中国航空无线电电子研究所 A kind of air navigation aid of radio auxiliary dead reckoning

Also Published As

Publication number Publication date
JPS58216910A (en) 1983-12-16

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