JPH0465323B2 - - Google Patents

Info

Publication number
JPH0465323B2
JPH0465323B2 JP15946383A JP15946383A JPH0465323B2 JP H0465323 B2 JPH0465323 B2 JP H0465323B2 JP 15946383 A JP15946383 A JP 15946383A JP 15946383 A JP15946383 A JP 15946383A JP H0465323 B2 JPH0465323 B2 JP H0465323B2
Authority
JP
Japan
Prior art keywords
signal
addition
latch
value
circuit
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
JP15946383A
Other languages
Japanese (ja)
Other versions
JPS6050411A (en
Inventor
Shuichi Kosuge
Kenji Kato
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.)
Denso Corp
Original Assignee
NipponDenso 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 NipponDenso Co Ltd filed Critical NipponDenso Co Ltd
Priority to JP15946383A priority Critical patent/JPS6050411A/en
Publication of JPS6050411A publication Critical patent/JPS6050411A/en
Publication of JPH0465323B2 publication Critical patent/JPH0465323B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/14Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by recording the course traversed by the object

Landscapes

  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Navigation (AREA)

Description

【発明の詳細な説明】 本発明は、車両、船舶等の移動体のための方位
演算装置に関する。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an azimuth calculation device for a moving object such as a vehicle or a ship.

従来、この種の方位演算装置としては、例え
ば、車両の進行方向の時間的角度変化、即ち角速
度をガスレートセンサにより検出するとともにこ
のガスレートセンサの検出結果を積分回路により
時間について積分し、この積分結果を当該車両の
進行方位に対応する値として利用するようにした
ものがある。しかしながら、かかる構成にあつて
は、積分時間が短かければ前記積分結果が精度の
よい値となつているものの、積分時間が長くなる
と、ガスレートセンサに固有のドリフト誤差に基
く前記積分結果の誤差が大きくなるという不具合
がある。
Conventionally, this type of azimuth calculation device detects, for example, a temporal angular change in the traveling direction of a vehicle, that is, an angular velocity, using a gas rate sensor, and integrates the detection result of the gas rate sensor over time using an integrating circuit. Some systems use the integration result as a value corresponding to the traveling direction of the vehicle. However, in such a configuration, if the integration time is short, the integration result is a highly accurate value, but if the integration time is long, an error in the integration result based on the drift error inherent to the gas rate sensor increases. There is a problem that becomes large.

本発明はこのようなことに対処してなされたも
ので、その目的とするところは、上述したドリフ
ト誤差の影響を受けることなく移動体の進行方位
を精度よく演算するようにした移動体のための方
位演算装置を提供することにある。
The present invention has been made in response to the above-mentioned problems, and its purpose is to accurately calculate the heading direction of a moving object without being affected by the above-mentioned drift error. The object of the present invention is to provide an azimuth calculation device.

かかる目的の達成にあたり、本発明の構成上の
特徴は、移動体の進行方向の時間的角度変化を第
1方位角度として検出する第1検出手段と、移動
体の進行方向の地磁気方向に対する角度差を第2
方位角度として検出する第2検出手段と、経時的
にパルス信号を繰返し発生するパルス信号発生手
段と、移動体の進行方位に対応する第1加算値を
求める第1加算手段と、前記パルス信号発生手段
からの先行パルス信号に応答して前記第2方位角
度と前記第1加算値との差を演算するとともにこ
の演算結果に定数(<1)を乗じる演算手段と、
第2加算値を求める第2加算手段と、前記パルス
信号発生手段からの後行パルス信号に応答して前
記第2加算値をラツチするラツチ手段とを設け
て、前記第2加算手段が前記演算手段による乗算
結果を前記ラツチ手段による第2ラツチ加算値に
加算してこの加算結果を前記第2加算値とし、か
つ前記第1加算手段が前記後行パルス信号に応答
して前記第1方位角度に前記第2ラツチ加算値を
加算しこの加算結果を前記第1加算値とするよう
にしたことにある。
In order to achieve such an object, the structural features of the present invention include a first detection means for detecting a temporal angular change in the moving direction of the moving body as a first azimuth angle, and a first detection means for detecting a temporal angular change in the moving direction of the moving body, and an angular difference between the moving direction of the moving body and the geomagnetic direction. the second
a second detection means for detecting as an azimuth angle; a pulse signal generation means for repeatedly generating a pulse signal over time; a first addition means for obtaining a first addition value corresponding to the traveling direction of the moving object; and the pulse signal generation means. calculating means for calculating the difference between the second azimuth angle and the first added value in response to a preceding pulse signal from the means, and multiplying the calculation result by a constant (<1);
A second addition means for calculating a second addition value and a latch means for latching the second addition value in response to a trailing pulse signal from the pulse signal generation means are provided, and the second addition means calculates the second addition value. The multiplication result by the means is added to the second latch addition value by the latch means, and the addition result is used as the second addition value, and the first addition means responds to the trailing pulse signal to calculate the first azimuth angle. The second latch addition value is added to the second latch addition value, and the addition result is used as the first addition value.

しかして、このように本発明を構成したことに
より、前記第1加算値が、初期値の(1−α)m
の積と前記第2方位角度との和により決定される
ので、mが前記パルス信号の発生数の増大に伴い
増大したとき(1−α)mが零に近ずき、その結
果、前記第1加算値が前記第2方位角度に実質的
に等しくなる。このことは、前記第1検出手段に
固有のドリフト誤差に基く前記第1方位角度の誤
差が、時間の経過に応じて増大しても、これに影
響されることなく前記第2方位角度によつて移動
体の進行方位を特定し得ることを意味する。
By configuring the present invention in this way, the first addition value is determined by the sum of the product of the initial value (1-α) m and the second azimuth angle, so that m is As the number of generated pulse signals increases, (1-α) m approaches zero, and as a result, the first added value becomes substantially equal to the second azimuth angle. This means that even if the error in the first azimuth angle based on the drift error inherent in the first detection means increases over time, the error in the second azimuth angle will not be affected by this. This means that the moving direction of the moving body can be specified.

以下、本発明の一実施例を図面により説明する
と、図面は、本発明に係る車両用方位演算装置の
ブロツク回路を示しており、この方位演算装置
は、角速度センサ10及び地磁気センサ20と、
これら角速度センサ10及び地磁気センサ20に
それぞれ接続した積分回路30及び変換回路40
を備えている。角速度センサ10は、レートジヤ
イロ、ガスレートセンサ等からなるもので、当該
車両の進行方位の時間的角度変化を検出しこの検
出結果を角速度信号として発生する。地磁気セン
サ20は、当該車両の進行方位の真北(即ち、地
磁気の方向)に対する方位差を第1と第2の座標
成分として検出しこれら第1と第2の座標成分を
それぞれ第1と第2の方位成分信号として発生す
る。積分回路30は、角速度センサ10からの角
速度信号に応答してこの信号の値を時間について
デイジタル的に積分しこの積分結果をデイジタル
方位信号として発生する。変換回路40は、地磁
気センサ20からの第1と第2の方位成分信号に
応答してこれら両信号の値の比をデイジタル的に
計算しこの計算結果をデイジタル方位信号として
発生する。
Hereinafter, one embodiment of the present invention will be described with reference to the drawings. The drawings show a block circuit of a vehicle azimuth calculation device according to the present invention, and this azimuth calculation device includes an angular velocity sensor 10, a geomagnetic sensor 20,
An integrating circuit 30 and a conversion circuit 40 are connected to the angular velocity sensor 10 and the geomagnetic sensor 20, respectively.
It is equipped with The angular velocity sensor 10 is composed of a rate gyro, a gas rate sensor, etc., and detects a temporal angular change in the traveling direction of the vehicle, and generates the detection result as an angular velocity signal. The geomagnetic sensor 20 detects the difference in orientation of the vehicle's traveling direction with respect to due north (i.e., the direction of geomagnetism) as first and second coordinate components, and converts these first and second coordinate components into first and second coordinate components, respectively. It is generated as two azimuth component signals. Integrating circuit 30 responds to the angular velocity signal from angular velocity sensor 10, digitally integrates the value of this signal over time, and generates the integration result as a digital azimuth signal. The conversion circuit 40 digitally calculates the ratio of the values of these two signals in response to the first and second azimuth component signals from the geomagnetic sensor 20, and generates the calculation result as a digital azimuth signal.

また、方位演算装置は、走行距離センサ50
と、この走行距離センサ50に接続した整形回路
60と、積分回路30及び整形回路60に接続し
たラツチ回路70と、変換回路40及び整形回路
60に接続したラツチ回路80を備えており、走
行距離センサ50は当該車両の単位走行距離毎に
これを検出しこれら各検出結果を、順次、走行距
離信号αo(n=1、2、……)として発生する。
整形回路60は走行距離センサ50からの各走行
距離信号αoを順次波形整形し整形信号boとして発
生する。ラツチ回路70は整形回路60からの各
整形信号boに応答して積分回路30からのデイジ
タル方位信号を順次ラツチしこれら各デイジタル
方位信号の値(以下、進行方位oと称する)を
ラツチ方位信号として発生する。ラツチ回路80
は、整形回路60からの各整形信号boに応答して
変換回路40からのデイジタル方位信号を順次ラ
ツチしこれら各デイジタル信号の値(以下、進行
方位Doと称する)をラツチ方位信号として発生
する。
Further, the azimuth calculation device includes a mileage sensor 50
A shaping circuit 60 connected to the mileage sensor 50, a latch circuit 70 connected to the integrating circuit 30 and the shaping circuit 60, and a latch circuit 80 connected to the conversion circuit 40 and the shaping circuit 60 are provided. The sensor 50 detects this for each unit mileage of the vehicle, and sequentially generates each detection result as a mileage signal α o (n=1, 2, . . . ).
The shaping circuit 60 sequentially shapes the waveform of each mileage signal α o from the mileage sensor 50 and generates a shaped signal b o . The latch circuit 70 sequentially latches the digital azimuth signals from the integrating circuit 30 in response to each shaping signal bo from the shaping circuit 60, and converts the value of each digital azimuth signal (hereinafter referred to as heading o ) into a latched azimuth signal. occurs as. Latch circuit 80
latches the digital azimuth signals from the conversion circuit 40 in response to each shaping signal b o from the shaping circuit 60, and generates the value of each digital signal (hereinafter referred to as heading azimuth D o ) as a latched azimuth signal. do.

また、方位演算装置は、ラツチ回路70及びラ
ツチ回路130に接続した加算器90と、ラツチ
回路80及び加算器90に接続した減算器100
と、この減算器100及び定数設定回路110a
に接続した乗算器110と、この乗算器110及
びラツチ回路130に接続した加算器120を備
えており、加算器90はラツチ回路70からのラ
ツチ方位信号の値oをラツチ回路130から後
述のごとく生じるラツチ加算信号の値φoに加算
しこの加算結果(θoo+φo)を出力方位信号と
して発生する。減算器100はラツチ回路80か
らのラツチ方位信号の値Doから加算器90から
の出力方位信号の値θoを減算しこの減算結果
(Do−θo=Doo−φo)を減算信号として発生す
る。
The azimuth calculation device also includes an adder 90 connected to the latch circuit 70 and the latch circuit 130, and a subtracter 100 connected to the latch circuit 80 and the adder 90.
And this subtracter 100 and constant setting circuit 110a
, and an adder 120 connected to the multiplier 110 and the latch circuit 130. It is added to the value φ o of the resulting latch addition signal, and the addition result (θ o = o + φ o ) is generated as an output azimuth signal. The subtracter 100 subtracts the value θ o of the output azimuth signal from the adder 90 from the value D o of the latch azimuth signal from the latch circuit 80 , and obtains the result of this subtraction (D o −θ o =D oo −φ o ). is generated as a subtraction signal.

定数設定回路110aは定数αを設定信号とし
て発生するもので、この設定信号の値αは、当該
車両の走行距離との関連におけるラツチ方位信号
の値oのラツチ方位信号の値Doへの収束度合を
表わす。本実施例においては、当該車両の走行距
離が数100mにてoがDoに収束するように0<α
<1として選定されている。乗算器110は減算
器100からの減算信号の値(Do−θo)を定数
設定回路110aからの設定信号の値αに乗じこ
の乗算結果α(Do−θo)を乗算信号として発生す
る。加算器120は乗算器110からの乗算信号
の値α(Do−θo)にラツチ回路130からのラツ
チ加算信号の値φoを加算しこの加算結果{α(Do
−θo)+φo}を加算信号として発生する。ラツチ
回路130は、整形回路60からの整形信号bo
応答して加算器120からの加算信号をラツチ
し、この加算信号の値{α(Do-1−θo-1)+φo-1
=φoをラツチ加算信号として発生するとともに、
整形回路60からの整形信号bo+1に応答して加算
器120からの前記加算信号に後続する加算信号
をラツチし、この加算信号の値{α(Do−θo)+
φo}=φo+1を前記ラツチ加算信号に後続するラツ
チ加算信号として発生する。
The constant setting circuit 110a generates a constant α as a setting signal, and the value α of this setting signal is determined by the convergence of the value o of the latch azimuth signal to the value D o of the latch azimuth signal in relation to the traveling distance of the vehicle. Represents degree. In this example, 0 < α
<1. The multiplier 110 multiplies the value of the subtraction signal (D o −θ o ) from the subtracter 100 by the value α of the setting signal from the constant setting circuit 110a, and generates this multiplication result α (D o −θ o ) as a multiplication signal. do. The adder 120 adds the value φ o of the latch addition signal from the latch circuit 130 to the value α(D o −θ o ) of the multiplication signal from the multiplier 110, and the addition result {α(D o
−θ o )+φ o } is generated as an addition signal. The latch circuit 130 latches the addition signal from the adder 120 in response to the shaping signal bo from the shaping circuit 60, and the value of this addition signal {α(D o-1 −θ o-1 )+φ o- 1 }
o is generated as a latch addition signal, and
In response to the shaping signal b o+1 from the shaping circuit 60, the addition signal subsequent to the addition signal from the adder 120 is latched, and the value of this addition signal {α(D o −θ o )+
φ o }=φ o+1 is generated as a latch addition signal following the latch addition signal.

ところで、ラツチ回路130からのラツチ加算
信号の値φoを数学的に検討してみると、n=1、
2、……においてDo=D、o=とすれば、 φo=α(D−−φo-1)+φo-1 ……(1) この(1)式を次のように変形すれば φo−(D− =α(D−−φo-1)−(D−)+φo-1 =(1−α){φo-1−(D−)} =(1−α)2{φo-2−(D−)} …… =(1−α)n-1{φ1−(D−)} ……(2) が得られる。従つて、この(2)式において、0<α
<1を考慮してn→∞とすれば、(1−α)n-1
0故 φo+=D ……(3) が成立する。このことは、整形回路60からの整
形信号boの発生数の増大に伴い加算器90の出力
方位信号の値θoo+φo=+φoがラツチ回路
80からのラツチ方位信号の値Do=Dに収束し
て行くことを意味する。
By the way, when we consider mathematically the value φ o of the latch addition signal from the latch circuit 130, we find that n=1,
2. If D o = D, o = in ..., φ o = α (D−−φ o-1 ) + φ o-1 ...(1) Transform equation (1) as follows. For example, φ o -(D- = α(D--φ o-1 )-(D-) + φ o-1 = (1-α) {φ o-1 −(D-)} = (1-α) 2o-2 −(D−)} ...=(1−α) n-11 −(D−)} ...(2) is obtained. Therefore, in this equation (2), ,0<α
Considering <1 and let n→∞, (1-α) n-1
0, so φ o +=D ...(3) holds true. This means that as the number of shaping signals b o generated from the shaping circuit 60 increases, the value θ o = oo = +φ o of the output orientation signal of the adder 90 increases as the value D of the latch orientation signal from the latch circuit 80 increases. This means that o = convergence to D.

以上のように構成した本実施例において、当該
車両を走行させるとともに本発明装置を作動させ
れば、積分回路30が角速度センサ10との協働
によりデイジタル方位信号を発生し、変換回路4
0が地磁気センサ20との協働によりデイジタル
方位信号を発生する。かかる段階にて、整形回路
60が、走行距離センサ50から生じる走行距離
信号ao-1に応答して整形信号bo-1を生じると、こ
の整形信号bo-1が各ラツチ回路70,80,13
0に付与される。すると、ラツチ回路70が整形
信号bo-1に応答して積分回路30からのデイジタ
ル方位信号をラツチするとともにこの信号の値
o-1をラツチ方位信号として発生し加算器90に
付与する。
In this embodiment configured as described above, when the vehicle is driven and the device of the present invention is activated, the integrating circuit 30 generates a digital azimuth signal in cooperation with the angular velocity sensor 10, and the converting circuit 4
0 generates a digital azimuth signal in cooperation with the geomagnetic sensor 20. At this stage, when the shaping circuit 60 generates a shaping signal b o-1 in response to the mileage signal a o-1 generated from the mileage sensor 50, this shaping signal b o-1 is transmitted to each latch circuit 70, 80,13
Assigned to 0. Then, the latch circuit 70 latches the digital azimuth signal from the integrating circuit 30 in response to the shaping signal b o-1 and changes the value of this signal.
o-1 is generated as a latch orientation signal and applied to adder 90.

また、ラツチ回路80が整形回路60からの整
形信号bo-1に応答して変換回路40からのデイジ
タル方位信号をラツチするとともにこの信号の値
Do-1をラツチ方位信号として減算器100に付
与し、これと同時に、ラツチ回路130が、加算
器120から先行して発生している加算信号をラ
ツチするとともにこの加算信号の値φo-1={α
(Do-2−θo-2)+φo-2}をラツチ加算信号として両
加算器90,120に付与する。すると、加算器
90がラツチ回路70からのラツチ方位信号の値
o-1にラツチ回路130からのラツチ加算信号の
値φo-1を加算するとともにこの加算結果(θo-1
o-1+φo-1)を出力方位信号として発生し減算器
100に付与する。
Further, the latch circuit 80 latches the digital azimuth signal from the conversion circuit 40 in response to the shaping signal b o-1 from the shaping circuit 60, and also latches the value of this signal.
D o-1 is applied to the subtracter 100 as a latch azimuth signal, and at the same time, the latch circuit 130 latches the addition signal generated in advance from the adder 120, and the value of this addition signal φ o- 1 = {α
(D o-2 −θ o-2 )+φ o-2 } is applied to both adders 90 and 120 as a latch addition signal. Then, the adder 90 receives the value of the latch direction signal from the latch circuit 70.
The value φ o-1 of the latch addition signal from the latch circuit 130 is added to o-1 , and the addition result (θ o-1 =
o-1o-1 ) is generated as an output azimuth signal and applied to the subtracter 100.

ついで、減算器100が加算器90からの出力
方位信号の値θo-1をラツチ回路80からのラツチ
方位信号の値Do-1から減算しこの減算結果
(Do-1−θo-1)を減算信号として発生し、乗算器
110が、定数設定回路110aからの設定信号
の値αを減算器100からの減算信号の値
(Do-1−θo-1)に乗じこの乗算結果α(Do-1
θo-1)を乗算信号として発生し、かつ加算器12
0がかかる乗算信号の値α(Do-1−θo-1)をラツ
チ回路130からのラツチ加算信号の値φo-1に加
算しこの加算結果{α(Do-1−θo-1)+φo-1}を加
算信号として発生する。
Next, the subtracter 100 subtracts the value θ o-1 of the output azimuth signal from the adder 90 from the value D o-1 of the latch azimuth signal from the latch circuit 80, and the subtraction result (D o-1 −θ o- 1 ) is generated as a subtraction signal, and the multiplier 110 multiplies the value α of the setting signal from the constant setting circuit 110a by the value (D o-1 −θ o-1 ) of the subtraction signal from the subtracter 100, and performs this multiplication. Result α(D o-1
θ o-1 ) is generated as a multiplication signal, and the adder 12
The value α(D o-1 −θ o-1 ) of the multiplication signal multiplied by 0 is added to the value φ o-1 of the latch addition signal from the latch circuit 130, and the addition result {α(D o-1 −θ o -1 ) +φ o-1 } is generated as an addition signal.

然る後、整形回路60が、走行距離センサ50
から生じる走行距離信号aoに応答して整形信号bo
を発生すると、この整形信号boが各ラツチ回路7
0,80,130に付与される。すると、ラツチ
回路70が整形回路60からの整形信号boに応答
して積分回路30からのデイジタル方位信号をラ
ツチするとともにこの信号の値oをラツチ方位
信号として発生し、これと同時に、ラツチ回路8
0が変換回路40からのデイジタル方位信号をラ
ツチするとともにこの信号の値Doをラツチ方位
信号として発生する。また、ラツチ回路130が
整形回路60からの整形信号boに応答して加算器
120からの加算信号の値φo={α(Do-1−θo-1
+φo-1}をラツチ加算信号として発生し、これに
伴い加算器90がラツチ回路70からのデイジタ
ル方位信号の値oにラツチ回路130からのラ
ツチ加算信号の値φoを加算しこの加算結果(θo
o+φo)を出力方位信号として発生する。この
ことは、上述の数学的検討結果から理解されると
おり、nの増大に応じて出力方位信号の値、即ち
当該車両の進行方位に対応する値がラツチ回路8
0からのラツチ方位信号の値に接近して実質的に
等しくなることを意味する。
After that, the shaping circuit 60 converts the mileage sensor 50
In response to the mileage signal a o resulting from the shaping signal b o
is generated, this shaped signal b o is sent to each latch circuit 7.
Granted to 0,80,130. Then, the latch circuit 70 latches the digital azimuth signal from the integrating circuit 30 in response to the shaping signal b o from the shaping circuit 60, and generates the value o of this signal as a latch azimuth signal. 8
0 latches the digital azimuth signal from conversion circuit 40 and generates the value D o of this signal as the latched azimuth signal. Further, the latch circuit 130 responds to the shaping signal b o from the shaping circuit 60 and calculates the value of the addition signal from the adder 120 φ o ={α(D o-1 −θ o-1 )
o-1 } is generated as a latch addition signal, and accordingly, the adder 90 adds the value φ o of the latch addition signal from the latch circuit 130 to the value o of the digital azimuth signal from the latch circuit 70, and the addition result is (θ o =
oo ) is generated as an output azimuth signal. As understood from the above mathematical study results, as n increases, the value of the output azimuth signal, that is, the value corresponding to the traveling azimuth of the vehicle, changes to the latch circuit 8.
This means that the value of the latch orientation signal from zero is close to and substantially equal to.

ところで、上述した作用説明において、当該車
両が、例えば交通渋滞により長時間に亘り同一の
地点にて停滞することとなつた場合には、走行距
離センサ50からの走行距離信号、即ち整形回路
60からの整形信号の発生が当該車両の停滞によ
り停止するため、各ラツチ回路70,80,13
0のラツチ内容が整形信号60からの整形信号の
発生停止直前の値に保持される。従つて、このよ
うな車両の停滞中に車両の周囲の磁界に乱れが生
じて変換回路40からのデイジタル方位信号の値
に地磁気センサ20固有の欠点に基く磁界の乱れ
による誤差が混入しても、これとはかかわりな
く、加算器90からの出力方位信号の値が、当該
車両の停滞直前における各ラツチ回路70,8
0,130のラツチ内容により適正に規定される
こととなる。また、このことは、磁界の乱れてい
る時間が長くなつても同様である。
By the way, in the above explanation of the operation, when the vehicle is stopped at the same point for a long time due to traffic congestion, the distance signal from the distance sensor 50, that is, the shaping circuit 60 Since generation of the shaping signal stops due to stagnation of the vehicle, each latch circuit 70, 80, 13
The content of the latch 0 is held at the value immediately before the generation of the shaping signal from the shaping signal 60 stopped. Therefore, even if the magnetic field around the vehicle is disturbed while the vehicle is stagnant and an error due to the disturbance of the magnetic field due to the inherent shortcomings of the geomagnetic sensor 20 is mixed into the value of the digital azimuth signal from the conversion circuit 40, , regardless of this, the value of the output azimuth signal from the adder 90 is the value of each latch circuit 70, 8 immediately before the vehicle stops.
It is properly defined by the latch contents of 0.130. This also applies even if the time during which the magnetic field is disturbed becomes longer.

なお、本発明の実施にあたつては、ラツチ回路
70,80,130、加算器90,120、減算
器100、乗算器110及び定数設定回路110
aに代えて、これらの各機能と同様の機能を果す
ようにプログラムしたマイクロコンピユータを採
用してもよいことは勿論である。
In addition, in implementing the present invention, latch circuits 70, 80, 130, adders 90, 120, subtracter 100, multiplier 110, and constant setting circuit 110
It goes without saying that a microcomputer programmed to perform the same functions as those described above may be used instead of a.

また、前記実施例においては、本発明を車両に
適用した例について説明したが、これに代えて、
例えば船舶等の移動体にも本発明を適用して実施
してもよい。
Further, in the above embodiment, an example in which the present invention is applied to a vehicle has been described, but instead of this,
For example, the present invention may also be applied to a moving body such as a ship.

また、前記実施例においては、ラツチ回路7
0,80,130の各ラツチ内容の更新手段とし
て、走行距離センサ50及び整形回路60を採用
した例について説明したが、これに代えて、一連
のクロツク信号を生じるクロツク回路を前記更新
手段として採用して実施してもよい。
Further, in the embodiment, the latch circuit 7
Although an example has been described in which the mileage sensor 50 and the shaping circuit 60 are used as means for updating the contents of the 0, 80, and 130 latches, instead of this, a clock circuit that generates a series of clock signals may be used as the updating means. It may also be carried out.

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

図面は本発明の一実施例を示すブロツク回路図
である。 符号の説明、10……角速度センサ、20……
地磁気センサ、30……積分回路、40……変換
回路、50……走行距離センサ、90,120…
…加算器、100……減算器、110……乗算
器、110a……定数設定回路、130……ラツ
チ回路。
The drawing is a block circuit diagram showing one embodiment of the present invention. Explanation of symbols, 10...Angular velocity sensor, 20...
Geomagnetic sensor, 30... Integrating circuit, 40... Conversion circuit, 50... Mileage sensor, 90, 120...
... Adder, 100 ... Subtractor, 110 ... Multiplier, 110a ... Constant setting circuit, 130 ... Latch circuit.

Claims (1)

【特許請求の範囲】[Claims] 1 移動体の進行方向の時間的角度変化を第1方
位角度として検出する第1検出手段と、移動体の
進行方向の地磁気方向に対する角度差を第2方位
角度として検出する第2検出手段と、経時的にパ
ルス信号を繰返し発生するパルス信号発生手段
と、移動体の進行方位に対応する第1加算値を求
める第1加算手段と、前記パルス信号発生手段か
らの先行パルス信号に応答して前記第2方位角度
と前記第1加算値との差を演算するとともにこの
演算結果に定数(<1)を乗じる演算手段と、第
2加算値を求める第2加算手段と、前記パルス信
号発生手段からの後行パルス信号に応答して前記
第2加算値をラツチするラツチ手段とを設けて、
前記第2加算手段が前記演算手段による乗算結果
を前記ラツチ手段による第2ラツチ加算値に加算
してこの加算結果を前記第2加算値とし、かつ前
記第1加算手段が前記後行パルス信号に応答して
前記第1方位角度に前記第2ラツチ加算値を加算
しこの加算結果を前記第1加算値とするようにし
た移動体のための方位演算装置。
1. A first detection means for detecting a temporal angular change in the moving direction of the moving body as a first azimuth angle, and a second detecting means for detecting an angular difference between the moving direction of the moving body and the geomagnetic direction as a second azimuth angle; pulse signal generating means for repeatedly generating a pulse signal over time; first adding means for calculating a first addition value corresponding to the traveling direction of the moving body; a calculation means for calculating the difference between the second azimuth angle and the first addition value and multiplying the calculation result by a constant (<1); a second addition means for calculating the second addition value; and a pulse signal generation means. latching means for latching the second added value in response to a trailing pulse signal;
The second addition means adds the multiplication result by the calculation means to the second latch addition value by the latch means, and sets the addition result as the second addition value, and the first addition means adds the result of the multiplication by the calculation means to the second latch addition value by the latch means, and An azimuth calculation device for a moving object, which responsively adds the second latch addition value to the first azimuth angle and uses the addition result as the first addition value.
JP15946383A 1983-08-31 1983-08-31 Azimuth operating device for moving body Granted JPS6050411A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15946383A JPS6050411A (en) 1983-08-31 1983-08-31 Azimuth operating device for moving body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15946383A JPS6050411A (en) 1983-08-31 1983-08-31 Azimuth operating device for moving body

Publications (2)

Publication Number Publication Date
JPS6050411A JPS6050411A (en) 1985-03-20
JPH0465323B2 true JPH0465323B2 (en) 1992-10-19

Family

ID=15694311

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15946383A Granted JPS6050411A (en) 1983-08-31 1983-08-31 Azimuth operating device for moving body

Country Status (1)

Country Link
JP (1) JPS6050411A (en)

Also Published As

Publication number Publication date
JPS6050411A (en) 1985-03-20

Similar Documents

Publication Publication Date Title
US4673878A (en) Vehicle location display device with averaging means for correcting location information
US4416067A (en) Correction method and device for a magnetic field probe
CN107990910A (en) A kind of naval vessel Large azimuth angle Transfer Alignment based on volume Kalman filtering
ES8306536A1 (en) Navigation system.
CA1093662A (en) Shipboard reference for an aircraft navigation system
US3952187A (en) Circuit for transforming rectangular coordinates to polar coordinates
CN111207776A (en) Star sensor and gyroscope combined calibration method suitable for Mars detection
JPS60135814A (en) Azimuth detecting apparatus
JP2000337925A (en) R/d converter
JPH0465323B2 (en)
JPH0694734A (en) Drift cancel system and apparatus for angular velocity detecting sensor
US4584652A (en) Apparatus and method for determining in-phase and quadrature-phase components
RU2098322C1 (en) Complex compass system
JPH0949737A (en) Navigation signal output method
JPH03285110A (en) Measuring apparatus of angular velocity
RU2154810C2 (en) Gimballess attitude control system
JP3303174B2 (en) On-board positioning device
JPS61155813A (en) Estimating device for position of moving body
Bayard Reduced-order kalman filtering with relative measurements
JP3303175B2 (en) On-board positioning device
JP2743365B2 (en) Radar tracking filter method
JPS61231411A (en) Apparatus for measuring position of vehicle
EP0541223A1 (en) Vehicle-direction detecting apparatus
JP2756554B2 (en) Inertial device
JPS6480891A (en) Radar/chart information display device