JPS6118999U - landing guidance system - Google Patents
landing guidance systemInfo
- Publication number
- JPS6118999U JPS6118999U JP10409984U JP10409984U JPS6118999U JP S6118999 U JPS6118999 U JP S6118999U JP 10409984 U JP10409984 U JP 10409984U JP 10409984 U JP10409984 U JP 10409984U JP S6118999 U JPS6118999 U JP S6118999U
- Authority
- JP
- Japan
- Prior art keywords
- data
- target
- aircraft
- targets
- guidance system
- 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
Links
Landscapes
- Radar Systems Or Details Thereof (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図は、本考案の基本構成を示したブロック図、第２
図〜第４図は本考案の原理を説明するための図である。
ＩＡ，ＩＢ・・・・・・目標（リフレクタ）、２・・・
・・・センサ、３・・・・・・高度計、４・・・・・・
演算装置。Figure 1 is a block diagram showing the basic configuration of the present invention.
4 to 4 are diagrams for explaining the principle of the present invention. IA, IB...Target (reflector), 2...
...Sensor, 3...Altimeter, 4...
Computing device.
Claims (1)
した複数の目標物からなる地上部分と、前記目標物と自
機との相対距離及び高度を電波を放射することによって
測定するセンサと演算部とからなる機上部分から構成さ
れる着陸誘導装置において、前記目標物との相対距離差
の測定値によって目標を区別し、既知の各目標物の座標
データと、各目標物と自機との押対距離データ及び自機
の高度データとを組合せることによって３次元位置デー
タと予め定めた基準経路からの偏差データを求め、更に
前記各目標物の座標データと自機の３次元位置データと
から目標物の方向を予測し、前記目標物の予測方向と機
首方位角と機首方位角と姿勢角データとの和又は差をと
ることによって機首を基準とする目標物の方向を計算し
、前記機首を基準とする目標物の方向の計算結果を設定
値とし、前記センサの電波放射ビーム方向をフィードバ
ック自動制御することを特徴とする着陸誘導装置。A ground section consisting of a plurality of targets arranged obliquely to the runway centerline at predetermined positions near the runway, and a sensor that measures the relative distance and altitude between the targets and the own aircraft by emitting radio waves. In the landing guidance system, which consists of an upper part of the aircraft consisting of a calculation section, targets are distinguished based on the measured value of the relative distance difference with the target, and the coordinate data of each known target and the coordinate data of each target and the own aircraft are identified. The three-dimensional position data and the deviation data from the predetermined reference route are determined by combining the pushing distance data and the altitude data of the own aircraft, and the coordinate data of each of the targets and the three-dimensional position of the own aircraft are determined. The direction of the target is predicted based on the data, and the direction of the target with respect to the nose is calculated by calculating the sum or difference of the predicted direction of the target, the heading angle, the heading angle, and the attitude angle data. A landing guidance system characterized in that the direction of the radio wave emission beam of the sensor is automatically controlled by feedback, using the calculated result of the direction of the target object with respect to the nose as a set value.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10409984U JPS6118999U (en) | 1984-07-10 | 1984-07-10 | landing guidance system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10409984U JPS6118999U (en) | 1984-07-10 | 1984-07-10 | landing guidance system |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6118999U true JPS6118999U (en) | 1986-02-03 |
Family
ID=30663463
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10409984U Pending JPS6118999U (en) | 1984-07-10 | 1984-07-10 | landing guidance system |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6118999U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2011240745A (en) * | 2010-05-14 | 2011-12-01 | Chugoku Electric Power Co Inc:The | Method for supporting landing of unmanned flying object and unmanned flying object |
| JP2017135832A (en) * | 2016-01-27 | 2017-08-03 | 株式会社ダイヘン | Movable body |
-
1984
- 1984-07-10 JP JP10409984U patent/JPS6118999U/en active Pending
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2011240745A (en) * | 2010-05-14 | 2011-12-01 | Chugoku Electric Power Co Inc:The | Method for supporting landing of unmanned flying object and unmanned flying object |
| JP2017135832A (en) * | 2016-01-27 | 2017-08-03 | 株式会社ダイヘン | Movable body |
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