JPH035097U - - Google Patents
Info
- Publication number
- JPH035097U JPH035097U JP6452189U JP6452189U JPH035097U JP H035097 U JPH035097 U JP H035097U JP 6452189 U JP6452189 U JP 6452189U JP 6452189 U JP6452189 U JP 6452189U JP H035097 U JPH035097 U JP H035097U
- Authority
- JP
- Japan
- Prior art keywords
- aircraft
- target
- information
- machine gun
- radar
- 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
- 238000010586 diagram Methods 0.000 description 3
Landscapes
- Radar Systems Or Details Thereof (AREA)
Description
第１図は、この考案の一実施例を示す構成図、
第２図は従来のレーダ射撃装置の構成図である。
図において１……機体、２……対空目標、３…
…レーダ装置、４……セントラルコンピユータ、
５……慣性航法装置、６……表示器、７……パイ
ロツト、８……操縦コンピユータ、９……機体姿
勢制御器、１０……発射管制器、１１……機関砲
である。なお、図中、同一あるいは相当部分には
同一符号を付して示してある。
FIG. 1 is a configuration diagram showing an embodiment of this invention.
FIG. 2 is a block diagram of a conventional radar shooting device. In the diagram, 1... aircraft, 2... anti-aircraft target, 3...
...Radar equipment, 4...Central computer,
5... Inertial navigation device, 6... Display device, 7... Pilot, 8... Control computer, 9... Aircraft attitude controller, 10... Launch control device, 11... Machine gun. In the drawings, the same or corresponding parts are denoted by the same reference numerals.
Claims (1)
レーダ装置において、目標情報を出力するレーダ
装置と、機体姿勢情報を出力する慣性航法装置と
各々からの情報で機関砲弾道の見越し角を計算す
るセントラルコンピユータとその見越し角で機関
法の弾が目標に命中するように機体姿勢を計算す
る操縦コンピユータとその出力で機体を制御する
機体姿勢制御器と、レーダ装置の情報を表示する
表示器で、パイロツトが目標を補捉すると上記で
自動目標追尾状態のとき機関砲の照準が自動的に
目標に定まるように機体を制御し、自動的に機関
砲を発射するように構成されていることを特徴と
するレーダ射撃装置。 In a radar device that has a target tracking function for an aircraft equipped with a machine gun, a radar device that outputs target information, an inertial navigation device that outputs aircraft attitude information, and a central computer that calculates the expected angle of the machine gun trajectory using information from each. A pilot computer calculates the attitude of the aircraft so that the engine's bullet will hit the target at the expected angle, an aircraft attitude controller that controls the aircraft with its output, and a display that displays information from the radar system. When a target is detected, the machine is configured to control the aircraft so that the machine gun is automatically aimed at the target in the automatic target tracking state as described above, and to automatically fire the machine gun. radar shooting device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6452189U JPH035097U (en) | 1989-06-02 | 1989-06-02 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6452189U JPH035097U (en) | 1989-06-02 | 1989-06-02 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPH035097U true JPH035097U (en) | 1991-01-18 |
Family
ID=31595543
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6452189U Pending JPH035097U (en) | 1989-06-02 | 1989-06-02 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH035097U (en) |
-
1989
- 1989-06-02 JP JP6452189U patent/JPH035097U/ja active Pending
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4004487A (en) | Missile fire-control system and method | |
| US8450668B2 (en) | Optically guided munition control system and method | |
| EP2593744B1 (en) | Optoelectronic digital apparatus for assisting an operator in determining the shooting attitude to be given to a hand-held grenade launcher so as to strike a moving target, and respective operation method | |
| US5465212A (en) | Helicopter integrated fire and flight control having a pre-launch and post-launch maneuver director | |
| US3992708A (en) | Optical tracking analog flywheel | |
| US20060219094A1 (en) | Real time dynamically controled elevation and azimuth gun pod mounted on a fixed wing aerial combat vehicle | |
| EP0641464B1 (en) | Helicopter integrated fire and flight control having constraint limiting control | |
| US4086841A (en) | Helical path munitions delivery | |
| US4308015A (en) | System and method for aircraft gunnery training and accuracy evaluation | |
| JPH0319480B2 (en) | ||
| EP0667005B1 (en) | Helicopter integrated fire and flight control having coordinated area bombing control | |
| JPH035097U (en) | ||
| US20230140441A1 (en) | Target acquisition system for an indirect-fire weapon | |
| KR102318621B1 (en) | Attitude control method and attitude control system for wehicle mounted remote control weapon system | |
| JPH0357400B2 (en) | ||
| JPH01147299A (en) | Firearm control system for loading on aircraft | |
| RU2150064C1 (en) | Self-propelled gun (modifications) | |
| JPS63104899U (en) | ||
| JP2645059B2 (en) | Flying object guidance device | |
| RU2662766C1 (en) | Method for provision of the group of portable anti-aircraft missile systems shooting automation and device for its implementation | |
| JPH0415498A (en) | Guiding method missile | |
| JPS5848840B2 (en) | Hishiyoutaino Kuuchiyuurotsukuonhoushiki | |
| CROSE | A development and demonstration program on low cost inertial guidance for tactical weapon system applications(Low cost inertial guidance system commands missile attitude so that modified ballistic trajectory is followed along direct line of sight to target) | |
| JPS58129200A (en) | Antiaircraft controller | |
| JPH05264200A (en) | Control method of seeker for missile |