JPH03112678U - - Google Patents

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Publication number
JPH03112678U
JPH03112678U JP1690890U JP1690890U JPH03112678U JP H03112678 U JPH03112678 U JP H03112678U JP 1690890 U JP1690890 U JP 1690890U JP 1690890 U JP1690890 U JP 1690890U JP H03112678 U JPH03112678 U JP H03112678U
Authority
JP
Japan
Prior art keywords
launcher
sensors
sensor
controller
actuator
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
JP1690890U
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 JP1690890U priority Critical patent/JPH03112678U/ja
Publication of JPH03112678U publication Critical patent/JPH03112678U/ja
Pending legal-status Critical Current

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  • Toys (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Description

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

第1図はこの考案の実施例を示す図、第2図は
この考案のGセンサの検出方法を示す図、第3図
はこの考案の制御器のブロツク図、第4図は従来
のランチヤシステムを示す図、第5図は従来の垂
直ランチヤシステムを示す図である。 1……ランチヤ、2……走行車両、4a……G
センサA、4b……GセンサB、5……アクチユ
エータ、6……制御器である。なお、図中同一符
号は同一、又は相当部分を示す。
Fig. 1 is a diagram showing an embodiment of this invention, Fig. 2 is a diagram showing a detection method of the G sensor of this invention, Fig. 3 is a block diagram of a controller of this invention, and Fig. 4 is a diagram of a conventional launcher. FIG. 5 is a diagram showing a conventional vertical launcher system. 1... Lancia, 2... Traveling vehicle, 4a...G
Sensor A, 4b...G sensor B, 5... actuator, 6... controller. Note that the same reference numerals in the figures indicate the same or equivalent parts.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 走行車両に搭載された誘導飛しよう体のランチ
ヤにおいて、ランチヤ上に軸方向及び軸直角方向
に各々重力センサ(Gセンサ)を取り付けた構造
と前記Gセンサの出力でランチヤの傾き角を制御
するためのアクチユエータと制御器を設けたこと
を特徴とするランチヤ。
In a launcher of a guided flying vehicle mounted on a traveling vehicle, a structure in which gravity sensors (G sensors) are mounted on the launcher in the axial direction and in an axis-perpendicular direction, and the inclination angle of the launcher is controlled by the output of the G sensor. A launcher characterized by being equipped with an actuator and a controller.
JP1690890U 1990-02-22 1990-02-22 Pending JPH03112678U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP1690890U JPH03112678U (en) 1990-02-22 1990-02-22

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP1690890U JPH03112678U (en) 1990-02-22 1990-02-22

Publications (1)

Publication Number Publication Date
JPH03112678U true JPH03112678U (en) 1991-11-18

Family

ID=31520149

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1690890U Pending JPH03112678U (en) 1990-02-22 1990-02-22

Country Status (1)

Country Link
JP (1) JPH03112678U (en)

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