JPS6438500U - - Google Patents

Info

Publication number
JPS6438500U
JPS6438500U JP13091487U JP13091487U JPS6438500U JP S6438500 U JPS6438500 U JP S6438500U JP 13091487 U JP13091487 U JP 13091487U JP 13091487 U JP13091487 U JP 13091487U JP S6438500 U JPS6438500 U JP S6438500U
Authority
JP
Japan
Prior art keywords
wing
actuator
control device
flying object
guided
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
JP13091487U
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 JP13091487U priority Critical patent/JPS6438500U/ja
Publication of JPS6438500U publication Critical patent/JPS6438500U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Description

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

第1図はこの考案における一実施例である誘導
飛しよう体の概略図、第2図はこの考案による誘
導飛しよう体の内部構造を示す断面図、第3図及
び第4図はこの考案による誘導飛しよう体の動作
の一例を示す概略図、第5図及び第6図は従来の
誘導飛しよう体を示す概略図、第7図、第8図、
第9図及び第10図は従来の誘導飛しよう体の動
作の一例を示す概略図である。 図において、2は前翼、3は主翼、4は後翼、
5は制御装置、6はアクチユエーターである。な
お、各図中、同一符号は同一または相当部分を示
す。
Figure 1 is a schematic diagram of a guided flying object that is an embodiment of this invention, Figure 2 is a sectional view showing the internal structure of the guided flying object according to this invention, and Figures 3 and 4 are based on this invention. A schematic diagram showing an example of the operation of a guided flying object, FIGS. 5 and 6 are schematic diagrams showing a conventional guided flying object, FIGS. 7 and 8,
FIGS. 9 and 10 are schematic diagrams showing an example of the operation of a conventional guided flying object. In the figure, 2 is the front wing, 3 is the main wing, 4 is the rear wing,
5 is a control device, and 6 is an actuator. In each figure, the same reference numerals indicate the same or corresponding parts.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 誘導飛しよう体の主翼の前方に設けた前翼と、
主翼の後方に設けた後翼と、操舵のための制御装
置と、上記制御装置の制御信号を受けて作動する
上記前翼のアクチユエータ及び上記後翼のアクチ
ユエーターとを備えた誘導飛しよう体。
A front wing provided in front of the main wing of the guided flight body,
A guided flying object comprising a rear wing provided behind the main wing, a control device for steering, and an actuator for the front wing and an actuator for the rear wing that operate in response to a control signal from the control device. .
JP13091487U 1987-08-28 1987-08-28 Pending JPS6438500U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP13091487U JPS6438500U (en) 1987-08-28 1987-08-28

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP13091487U JPS6438500U (en) 1987-08-28 1987-08-28

Publications (1)

Publication Number Publication Date
JPS6438500U true JPS6438500U (en) 1989-03-08

Family

ID=31386503

Family Applications (1)

Application Number Title Priority Date Filing Date
JP13091487U Pending JPS6438500U (en) 1987-08-28 1987-08-28

Country Status (1)

Country Link
JP (1) JPS6438500U (en)

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