JPS6354988U - - Google Patents

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Publication number
JPS6354988U
JPS6354988U JP14910486U JP14910486U JPS6354988U JP S6354988 U JPS6354988 U JP S6354988U JP 14910486 U JP14910486 U JP 14910486U JP 14910486 U JP14910486 U JP 14910486U JP S6354988 U JPS6354988 U JP S6354988U
Authority
JP
Japan
Prior art keywords
angle
flying object
stabilize
adjustment mechanism
azimuth
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
JP14910486U
Other languages
Japanese (ja)
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 JP14910486U priority Critical patent/JPS6354988U/ja
Publication of JPS6354988U publication Critical patent/JPS6354988U/ja
Pending legal-status Critical Current

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Description

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

第１図はこの考案の一実施例に係る飛翔体発射
装置を示す構成説明図、第２図は第１図の方位角
方向の調整動作を説明するために示した動作説明
図である。 １０……船舶、１１……発射台、１２……射角
調整機構、１３……飛翔体、１４……ジヤイロ、
１５……水面。 FIG. 1 is a configuration explanatory diagram showing a flying object launcher according to an embodiment of this invention, and FIG. 2 is an operational explanatory diagram shown to explain the adjustment operation in the azimuth direction of FIG. 1. 10... Ship, 11... Launch pad, 12... Shooting angle adjustment mechanism, 13... Flying object, 14... Gyro,
15...Water surface.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 飛翔安定用ジヤイロの搭載された飛翔体、この
飛翔体を支持して取付け物体に設置される発射台
と、発射台に設けられ前記飛翔体の高低角及び方
位角を調整する射角調整機構とを具備し、前記射
角調整機構により前記飛翔体の高低角を制御して
高低角方向の安定化を図り、かつ前記ジヤイロの
方位角に応じて前記射角調整機構を制御して方位
角方向の安定化を図るように構成したことを特徴
とする飛翔体発射装置。 A flying object on which a flight stabilization gyroscope is mounted, a launch pad that supports the flying object and is installed on an attached object, and a firing angle adjustment mechanism that is provided on the launch pad and adjusts the elevation angle and azimuth of the flying object. The elevation angle of the projectile is controlled by the angle of incidence adjustment mechanism to stabilize the elevation angle direction, and the angle of incidence adjustment mechanism is controlled according to the azimuth angle of the gyroscope to stabilize the height angle of the projectile in the azimuth direction. A flying object launcher characterized by being configured to stabilize the air.
JP14910486U 1986-09-29 1986-09-29 Pending JPS6354988U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP14910486U JPS6354988U (en) 1986-09-29 1986-09-29

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP14910486U JPS6354988U (en) 1986-09-29 1986-09-29

Publications (1)

Publication Number Publication Date
JPS6354988U true JPS6354988U (en) 1988-04-13

Family

ID=31063997

Family Applications (1)

Application Number Title Priority Date Filing Date
JP14910486U Pending JPS6354988U (en) 1986-09-29 1986-09-29

Country Status (1)

Country Link
JP (1) JPS6354988U (en)

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