JPS58193473A - Position measuring system for composite hyperbolic navigation - Google Patents

Position measuring system for composite hyperbolic navigation

Info

Publication number
JPS58193473A
JPS58193473A JP7549982A JP7549982A JPS58193473A JP S58193473 A JPS58193473 A JP S58193473A JP 7549982 A JP7549982 A JP 7549982A JP 7549982 A JP7549982 A JP 7549982A JP S58193473 A JPS58193473 A JP S58193473A
Authority
JP
Japan
Prior art keywords
hyperbolic navigation
data
information
moving object
accuracy
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.)
Pending
Application number
JP7549982A
Other languages
Japanese (ja)
Inventor
Masayuki Takahashi
正行 高橋
Tsuyoshi Arai
新井 強
Toshio Oikawa
及川 俊夫
Atsushi Okamura
岡村 厚始
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.)
SANKO KISEN KK
SENAA KK
Sanko Steamship Co Ltd
Original Assignee
SANKO KISEN KK
SENAA KK
Sanko Steamship 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 SANKO KISEN KK, SENAA KK, Sanko Steamship Co Ltd filed Critical SANKO KISEN KK
Priority to JP7549982A priority Critical patent/JPS58193473A/en
Publication of JPS58193473A publication Critical patent/JPS58193473A/en
Pending 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
    • G01S5/12Position-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 by co-ordinating position lines of different shape, e.g. hyperbolic, circular, elliptical or radial

Landscapes

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

Abstract

PURPOSE:To select a system allowing the decision of ships position at the highest accuracy from a plurality of systems different in characteristics in the effective coverage and the position decision accuracy by inputting rough positional information of a moving object when the position thereof is measured by respective system. CONSTITUTION:Receivers of a hyperbolic navigation assistance system different in characteristics in the effective coverage and the position decision accuracy, for example, a decca receiver 1, a loran receiver 2 and an omega receiver 3 are arranged. A signal converter 4 generalizes the form of output signals of the receivers 1, 2 and 3. A control processor 5 comprises a means 51 of temporarily storing output signals of the converter 4 for respective hyperbolic navigation assistance system, means 52 and 53 of switching signals of the means 51, a means 54 of computing signals or the like from the means 51 and a means 55 of controlling those means. A desplay 6 indicates the information from the device 5.

Description

【発明の詳細な説明】 本発明は櫓数シスデムで計測をbい、イの中から最適な
ものを選んで位置決定を行う複合双曲線航法測位システ
ムに関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a composite hyperbolic navigation and positioning system that performs measurements using a number of turret systems and selects the optimal one from among them to determine the position.

これまで、双曲線座標を用いて航行する船舶あるいは飛
行機等の移動体の位置決定を行う航行援助シテスムとし
ては、デツカ方式、ロランA方式、ロランC方式、オメ
ガ方式など、電波の到着時間差を利用した種々のシステ
ムが提案され、現実に運用段階に入っている。これらの
双曲線航行援助システムは、各方式によって有効通達範
囲と位置決定精度は興っている。一般に有効通達範囲の
広いものほどその位置決定精度は低くなっている。
Until now, navigation aid systems that use hyperbolic coordinates to determine the position of moving objects such as navigating ships or airplanes have utilized the difference in arrival time of radio waves, such as the Detsuka method, Loran A method, Loran C method, and Omega method. Various systems have been proposed and are actually in the operational stage. These hyperbolic navigational aid systems have varying effective coverage and positioning accuracy depending on their method. Generally, the wider the effective coverage area, the lower the positioning accuracy.

従って、船舶等の移動体の航行位置によってこれらの諸
方式の中のどれを使うかを決定することは重要な事であ
る。たとえば、外洋を航行している移動体では、精度を
多少犠牲にしてでも全世界規模でのサービスを可能とし
ているオメガ方式を選択し、近海あるいは沿岸を航行し
てる移動体では、サービス地域の広さより精度の高さを
重視してロランC方式、デツカ方式等を選択するのが一
般的であった。ここで各方式の精度は、電波の周波数、
伝播速度、位置線の交角や発散等によるだけではなく、
また方式を満足する精度を有する有効通達範囲は使用地
域の地理的条件、大気雑音等によっても影響を受けるた
め、その概略の位置のみで使用方式を決めた場合には必
ずしも最適な方式を選択できないうらみがあった。
Therefore, it is important to decide which of these methods to use depending on the navigational position of a moving object such as a ship. For example, a mobile object navigating the open ocean may choose the Omega method, which enables worldwide service even if it sacrifices some accuracy; It was common to choose the Loran C method, the Detsuka method, etc., with emphasis on high accuracy. Here, the accuracy of each method is the frequency of the radio wave,
Not only due to propagation speed, intersection angle and divergence of position lines, etc.
In addition, the effective notification range with accuracy that satisfies the method is also affected by the geographical conditions of the area of use, atmospheric noise, etc., so if the method to be used is determined only based on the approximate location, it is not necessarily possible to select the optimal method. I was jealous.

これまでの船舶あるいは航空機等に於ては、現在運用さ
れている双曲線航行援助システム中のどの方式を使った
場合に最も高精度で位置決定が行えるかをオペレータが
判断し、その方式による計測データをチャート上にプロ
ットすることによって移動体の位置決定を行っていた。
In the past, for ships and aircraft, operators judged which method among the hyperbolic navigation aid systems currently in use would allow for position determination with the highest accuracy, and the measurement data using that method was used. The position of the moving object was determined by plotting it on a chart.

従って使用する方式の選択は専らオペレータの能力と経
験に負うところとなり、行動範囲の広い利用者に於ては
不便なものであった。
Therefore, the selection of the method to be used depends solely on the ability and experience of the operator, which is inconvenient for users with a wide range of activities.

本発明はこの点に着目してなされたものであって、有効
通達範囲と位置決定1度が特徴的に異る複数の方式で位
置の計測を行ない、移動体の概略位置情報を入力するこ
とによって、これら複数のシステムの中から最も精度良
く位置決定できるシステムを選び出し、その誤差評価を
も行なう複合双曲線航法測位システムを提供することを
目的とするものであって、その要旨とするところは、前
記各方式によってデータの取込みおよびこれに基づく位
置データの計算処理を順次周期的に行う一方、その移動
体の概略位置情報を入力し、この概略位置情報に従って
前記各方式の優先順位を決定し、次いで、第1優先順位
の方式から順次、その方式が算出した位置データを基に
移動体の航跡に対応する基準線を導き出し、この11単
線からの前記位置データのバラツキを求め、これが所定
の幅に収まっているか否かを識別することで、その方式
による測位の適否を判定するとともに、そのバラツキに
基づいて誤差評価情報を作成することを特徴とする複合
双曲線航法測位システムに存する。
The present invention has been made with attention to this point, and the present invention measures the position using a plurality of methods with characteristically different effective notification ranges and position determination times, and inputs approximate position information of a moving object. The purpose of this project is to provide a composite hyperbolic navigation positioning system that selects the system that can determine the position with the highest accuracy from among these multiple systems and also evaluates its error. While sequentially and periodically performing data capture and calculation processing of position data based on the data using each of the methods, inputting general position information of the mobile object, and determining priority of each of the above methods according to this general position information, Next, in order from the method with the first priority, a reference line corresponding to the trajectory of the moving object is derived based on the position data calculated by the method, and the dispersion of the position data from these 11 single lines is determined. The present invention resides in a composite hyperbolic navigation positioning system characterized by determining the suitability of positioning by that method by identifying whether or not the method falls within the above range, and also creating error evaluation information based on the variation thereof.

以下図面に示す実施例に従って詳細に説明する。Embodiments will be described in detail below according to embodiments shown in the drawings.

第1図は本発明の一実施例を示すブロックダイ″″′5
1′T″″・msc*ri・2J5cに(、F3Ltt
   、+の有効通達範囲と位置決定1度とが特徴的に
異っている双曲線航行援助システムの受信機で、例えば
1はデツカ受信機、2はロフンc4i個機、3μオメガ
受信機である。4は各双曲線航行援助システムの受信1
11.2&3よび3の出力信号の形式を統一するための
信号変換装置である。5は第2図にその詳細を示すよう
に信号変iI!装置3の出り信号を各双曲線航行援助シ
ステム毎に一時蓄積しておく蓄積手段51、この蓄積手
段51の信号の切替を行う切替手段52および53.蓄
積手段51からの信号等を演算処理する演算処理手段5
4およびこれらの諸手段を制御する制御手段55によっ
て構成される1lilj御処Wl@瞳である。6はこの
制御処理装M5よりの情報を表示する表示装置、7は当
該船舶等の移動体の基地との通信のための通信端末装置
である。
FIG. 1 shows a block die ""'5 showing an embodiment of the present invention.
1'T''''・msc*ri・2J5c(,F3Ltt
, + are characteristically different in the effective communication range and the position determination degree. For example, 1 is a Decka receiver, 2 is a Rofun C4i receiver, and a 3μ Omega receiver. 4 is the reception of each hyperbolic navigation aid system 1
11. This is a signal conversion device for unifying the formats of the output signals of 2 & 3 and 3. 5 is a signal change iI! as shown in detail in FIG. Storage means 51 for temporarily storing output signals of the device 3 for each hyperbolic navigation aid system; switching means 52 and 53 for switching the signals of the storage means 51; Arithmetic processing means 5 for processing signals etc. from storage means 51
4 and a control means 55 for controlling these various means. 6 is a display device for displaying information from the control processing device M5, and 7 is a communication terminal device for communicating with the base of the mobile body such as the ship.

次に、この様に構成された複合双曲線航法測位システム
の動作を説明する。
Next, the operation of the composite hyperbolic navigation and positioning system configured in this manner will be explained.

先ず、信号変換装置4の端子Iに概略−位置情報5、時
刻情報等の初期値が入力される。と、各方式対応に初期
の緯度、経度の計算が行われる。この計算に要する時f
itはデツカの場合で約10秒、ロランCの場合で約8
秒、オメガの場合(°約15秒以内で終了する。ここ−
(・、この概略位置情報は移動体の航行位置を緯度、#
Ik度共M ”廣” el!度の精度(・表わしたもの
む”ある。徊号礎換@w14は(−の?/j期設定が終
了すると、各受信機1・−1うからの1ニー・夕を順次
取り込んで前述の対応づる初期の81眸11!14r利
用して夫々の11度、経度の!i1粋を周期的に管うう
5、この周期は約15秒&!慢ぐあって 各り式ごとの
計禅値は四−形式の信@に爽換され(デfンタル化され
て演算処ll!装置5に転送される。
First, initial values such as general position information 5, time information, etc. are input to terminal I of the signal conversion device 4. Then, initial latitude and longitude calculations are performed for each method. The time required for this calculation f
It is about 10 seconds for Detsuka and about 8 seconds for Loran C.
Seconds, for Omega (° Finishes within about 15 seconds.Here -
(・, This rough position information indicates the navigation position of the mobile object in latitude, #
Ik degree coM “Hiro” el! The degree of accuracy (・expressed) is ``. Using the initial correspondence of 81 eyes 11 and 14 r, we periodically calculate the 11 degrees and longitudes of each 11 degree and longitude.The period is about 15 seconds and the calculation value for each equation is It is converted into a 4-format message (digitalized and transferred to the arithmetic processing unit 5).

演算処理軸15では、この情報IFrI)楡十段b]に
一時蓄積し゛(おく、この蓄槽+設511於旬る情報の
蓄積は例えばh式別に酪楡1−リ/をjj+jc酪横さ
れる。即ら、倍号礎換装置4からの情報μm1iJ 1
11手段55の制御による切替手#1j52の働きによ
って対応づる蓄積1リアに格納される。Lこ(°。
In the arithmetic processing axis 15, this information is temporarily stored in the storage tank + equipment 511. That is, the information μm1iJ 1 from the multiple number conversion device 4
The data is stored in the corresponding storage 1 rear by the operation of the switch #1j52 under the control of the 11 means 55. Lko(°.

演算l1lJ御装置5の端子Cには、−j御に必殻な名
神のコマンドが入ツノされ、111 m11手段b5は
信号変換装置4から前記概略位WItI4報を演算処理
手段54へ転送させる。演算処理手段540、この概略
位置情報に基いて、受信機が設備されている双曲線航行
援助システム、即ち、デツカ、ロランC、オメガの各方
式中、位置決定精度の高さに応じて優先順位をつける。
A Meishin command, which is essential for -j control, is input to the terminal C of the arithmetic l1lJ control device 5, and the 111 m11 means b5 transfers the approximate position WItI4 information from the signal converter 4 to the arithmetic processing means 54. Based on this rough position information, the arithmetic processing means 540 prioritizes the hyperbolic navigation aid systems in which the receiver is installed, namely Detsuka, Loran C, and Omega, depending on the degree of positioning accuracy. Put on.

この優先順位の決定には、各方式の局座標、電波の周波
数、伝播速度さらには各方式固有のファクタ等を参酌し
て1稗によって求められる。これらの諸条件は全世界規
模で予め演算処理手段54内のメモリに記憶されている
。その結果、例えば、デツカ方式、ロラン方式、オメガ
方式類で優先順位が決まったとすると、これが制御手段
55へ返送される。
This priority order is determined in a simple manner by taking into consideration the station coordinates of each system, the frequency of radio waves, the propagation speed, and factors unique to each system. These conditions are stored in advance in the memory within the arithmetic processing means 54 on a worldwide scale. As a result, for example, if the priority order is determined among the Detsuka method, Loran method, and Omega method, this is sent back to the control means 55.

制御手段55はこの優先順位に従って切替手段53をI
ljwJLで蓄積手段51のデツカ方式に割当てられた
エリアより緯度、経度の計算結果を逐事続出し、演算処
理手段54へ送り、ここで当該移動体の航跡に対応する
基準線を導き出す。この作業は、前述の如く約15秒周
期で得られる緯度、経度の計算結果のデータの経時炭化
を統計的に処理して基準線を求めるものであって、例え
ばカルマンフィルタの手法あるいは、円、楕円等の2次
曲纏に近似する2次回帰、折れ輪に近似する1次回帰等
の手法によって求めることができる。第3図にAで示す
線がこの様にして導き出された基準線である。次に、演
算処理@[54はこの基準線Aの両側に所定の幅の誤差
領域Bを設定し、各計算結果のデータdがこの誤差領域
B内に収まっている場合には、この航行位置に於てはデ
ツカ方式が最適な双曲線航行援助システムであると判定
してこれを制御手段55へ知らせる。l1l一手段55
はこれによって演算処理手段54に前記81粋結果のデ
ータ双曲線航行援助システムの基準線Aからのバラツキ
の度合を統計的手法によって処理してその航行位置に於
けるWA差評価情報を作成するとともに、進行方向、ス
ピード、目的地までの距離等付帯的な事項の計算を行わ
せる。次にこれらの情報を表示装置6へ送り、使用方式
の名称、移動体の位置情報、その11I差評価情報、付
帯情報等を表示させるとともに、通信端末61117を
介してこれらの諸情報をその移動体が所aする基地の通
信   1局へも送信する。
The control means 55 controls the switching means 53 according to this priority order.
In ljwJL, the calculation results of latitude and longitude are successively obtained from the area assigned to the detsuka method of the storage means 51 and sent to the arithmetic processing means 54, where a reference line corresponding to the track of the mobile object is derived. As mentioned above, this work involves statistically processing the temporal carbonization of the latitude and longitude calculation result data obtained at approximately 15 second intervals to obtain a reference line. It can be determined by a method such as quadratic regression that approximates a quadratic curve, linear regression that approximates a folded ring, etc. The line indicated by A in FIG. 3 is the reference line derived in this way. Next, the calculation process @[54 sets an error region B of a predetermined width on both sides of this reference line A, and if the data d of each calculation result is within this error region B, the navigation position In this case, it is determined that the DETSKA method is the optimal hyperbolic navigation aid system, and this is notified to the control means 55. l1l one means 55
As a result, the arithmetic processing means 54 processes the degree of variation from the reference line A of the data hyperbolic navigation aid system of the 81 results using a statistical method, and creates WA difference evaluation information at that navigation position, Calculate incidental matters such as direction of travel, speed, distance to destination, etc. Next, this information is sent to the display device 6 to display the name of the usage method, location information of the moving object, its 11I difference evaluation information, additional information, etc., and this information is transferred via the communication terminal 61117. Communication of the base where the body is located also transmits to one station.

ここで、前記判別の結果、各計算結果のデータ双曲線航
行援助システムの中に誤差領域B内に収まらないものが
散見される場合にはこの航行位置に於てはデツカ方式は
必ずしも適した航行援助システムではないと判定し、こ
れを制御手段55へ知らせる。−)一手段55はこれに
よって切替手段53を制御して第2優先順位のロラン方
式に割当てられたエリアからデータを読み出し、演算処
理手段54へ転送する。次いで前記デツカ方式の場合と
全く同様に、導き出した基準線の誤差領域内にデータが
全て収まっているか否かを判別し、収まっていればロラ
ン方式が最適であると判定して前述の場合と同様の処理
を行い、収っていない場合には第3優先順位のオメガ方
式によって同様の処″理を行う。ここで、演算処理手段
54が計算した第1優先順位の方式が必ずしも最適な方
式とならないのは、その時の気象条件、地表波と空間波
との関係等によって、その航行位置に於ける条件が経時
的に変化するために起るものである。
Here, as a result of the above discrimination, if there are some data in the hyperbolic navigation aid system of each calculation result that do not fall within the error area B, then the Detsuka method is not necessarily a suitable navigation aid at this navigation position. It is determined that it is not a system, and this is notified to the control means 55. -) The means 55 thereby controls the switching means 53 to read data from the area assigned to the Loran method of the second priority, and transfers it to the arithmetic processing means 54. Next, in exactly the same way as in the case of the Detsuka method, it is determined whether all the data falls within the error range of the derived reference line, and if it does, it is determined that the Loran method is optimal, and the procedure is repeated as in the case described above. Similar processing is performed, and if the results are not satisfied, the same processing is performed using the omega method with the third priority.Here, the method with the first priority calculated by the arithmetic processing means 54 is not necessarily the optimal method. This is because the conditions at the navigation position change over time, depending on the weather conditions at that time, the relationship between surface waves and spatial waves, etc.

以上詳細に説明した様に、本発明の複合双曲線航法測位
システムによれば、航行位置の緯度、経度情報を度”の
騙位で概略的に入力してやるだけで、後は機械が自動的
に最適な方式を選び出し、その正確な位置情報が得られ
るばかりか、その位置情報のW/j4差押価まで行って
しまうものであるため、オペレータの能力、経験に負う
ところは非常に少ないものとなり、行動範囲の極めて広
い利用者に於てはその利用効果は顕著なものである。
As explained in detail above, according to the compound hyperbolic navigation positioning system of the present invention, simply input the latitude and longitude information of the navigation position roughly in degrees, and the machine will automatically do the rest. Not only can accurate position information be obtained by selecting a suitable method, but also the W/J4 seizure price of that position information is carried out, so there is very little dependence on the ability and experience of the operator, and it is difficult to take action. The effects of its use are remarkable among a wide range of users.

以上、自動的に処理が進行するシステムについて実施例
に基づいて説明したが、本発明の複合双曲線航法測位シ
ステムはこれにのみ限定されるものではなく、例えば、
各方式に於ける測位の適否判定毎にこれを表示@胃に表
示し、その方式で測位処理を行うか否かはオペレータが
入力する信号によってマニュアル的に決定されるもの等
、種々のバリエーションを含むものである。
Although the system in which processing automatically proceeds has been described based on the embodiments, the compound hyperbolic navigation positioning system of the present invention is not limited to this, for example,
Various variations are available, such as displaying the appropriateness of positioning for each method on the display@stomach, and manually determining whether or not to perform positioning processing using that method based on signals input by the operator. It includes.

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

lllIJ図は本発明の一実施例を示すブロックタイヤ
グラム、第2図はその制御処理装置の一例の構成を示す
ブロックダイヤグラム、第3図はその動作を説明するた
めの図である。 1.2.3・・・・・・双曲線航行援助システムの受信
機4・・・・・・信号変換輪重、5・・・・・・制御処
理装置、6・・・・・・表示装置、7・・・・・・通信
端末部属、51・・・・・・蓄積手段、52.53・・
・切替手段、54・・・・・・演算処理手段、55・・
・・・・制御手段、A・・・・・・基準線、B・・・・
・・誤差領域、d・・・・・・データ。 特 許 出願人 三光汽船株式会社 第1図 @2図 420− 第3i!i
FIG. 11IJ is a block diagram showing an embodiment of the present invention, FIG. 2 is a block diagram showing the configuration of an example of the control processing device, and FIG. 3 is a diagram for explaining its operation. 1.2.3...Hyperbolic navigation aid system receiver 4...Signal conversion wheel weight, 5...Control processing device, 6...Display device , 7... Communication terminal section, 51... Storage means, 52.53...
- Switching means, 54... Arithmetic processing means, 55...
... Control means, A ... Reference line, B ...
...Error area, d...Data. Patent Applicant Sanko Kisen Co., Ltd. Figure 1 @ Figure 2 420-3i! i

Claims (1)

【特許請求の範囲】[Claims] 複数の双曲線航行援助システムを用いて移動体の位置決
定を行う複合双曲線航法測位システムに於て、前記各り
式によってデータの取込みおよびこれに基づく位置デー
タの1韓処理を順次周期的に行う−h、その移動体の概
略位置情報を入力し、この概略位置情報に従って前記各
り式の優先触位を決定し、次いで、v111優先順位の
6式から順次、その方式が韓出した位1lf−夕を麺に
移動体の航跡に対応する基準線を導き出し、この11単
線からの前記位置データのバラツキを求め、これが所定
の幅に収まっているか否かを識別(ること(゛、イの6
式による測位の適否を判定するとともに、そのバラツキ
に基づいてw4差IN’価情報を作成りることを特徴と
する倹合双曲線航払測位シス1ム。
In a composite hyperbolic navigation positioning system that determines the position of a moving object using a plurality of hyperbolic navigation aid systems, data is taken in by each of the above formulas and position data is processed in sequence and periodically based on the data. h. Input the approximate position information of the moving object, determine the priority touch position of each of the above methods according to this general position information, and then sequentially select the priority position of each method from V111 priority order 1lf- In the evening, a reference line corresponding to the trajectory of the moving object is derived, the dispersion of the position data from these 11 single lines is determined, and it is determined whether or not this falls within a predetermined width (6).
1. A combined hyperbolic navigation positioning system characterized by determining the suitability of positioning using a formula and creating w4 difference IN' value information based on the variation thereof.
JP7549982A 1982-05-07 1982-05-07 Position measuring system for composite hyperbolic navigation Pending JPS58193473A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP7549982A JPS58193473A (en) 1982-05-07 1982-05-07 Position measuring system for composite hyperbolic navigation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP7549982A JPS58193473A (en) 1982-05-07 1982-05-07 Position measuring system for composite hyperbolic navigation

Publications (1)

Publication Number Publication Date
JPS58193473A true JPS58193473A (en) 1983-11-11

Family

ID=13578013

Family Applications (1)

Application Number Title Priority Date Filing Date
JP7549982A Pending JPS58193473A (en) 1982-05-07 1982-05-07 Position measuring system for composite hyperbolic navigation

Country Status (1)

Country Link
JP (1) JPS58193473A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6194786U (en) * 1984-11-26 1986-06-18
JP2018116368A (en) * 2017-01-16 2018-07-26 株式会社Soken Course recognition device

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS576313A (en) * 1980-06-14 1982-01-13 Japan Radio Co Ltd Display device of overall color wake
JPS5761909A (en) * 1980-09-25 1982-04-14 Furuno Electric Co Ltd Navigation device

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS576313A (en) * 1980-06-14 1982-01-13 Japan Radio Co Ltd Display device of overall color wake
JPS5761909A (en) * 1980-09-25 1982-04-14 Furuno Electric Co Ltd Navigation device

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6194786U (en) * 1984-11-26 1986-06-18
JP2018116368A (en) * 2017-01-16 2018-07-26 株式会社Soken Course recognition device

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