JPH0249800U - - Google Patents

Info

Publication number
JPH0249800U
JPH0249800U JP12790888U JP12790888U JPH0249800U JP H0249800 U JPH0249800 U JP H0249800U JP 12790888 U JP12790888 U JP 12790888U JP 12790888 U JP12790888 U JP 12790888U JP H0249800 U JPH0249800 U JP H0249800U
Authority
JP
Japan
Prior art keywords
satellite
despin
spin
reflector
communication antenna
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
JP12790888U
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 JP12790888U priority Critical patent/JPH0249800U/ja
Publication of JPH0249800U publication Critical patent/JPH0249800U/ja
Pending legal-status Critical Current

Links

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Control Of Position Or Direction (AREA)

Description

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

第1図は、この考案の一実施例であるスピン安
定型人工衛星のデスピンモータアセンブリが衛星
本体に固定された状態と、レーザピツクアツプの
出力するアンテナ位置パルス信号を示す図、第2
図は従来のスピン安定型人工衛星による、アンテ
ナ指向誤差検出方法を示す原理図、第3図は従来
のデスピンモータアセンブリの断面図である。図
に於て、1は地球、2はデスピン部、3は衛星本
体部、4は地球センサ、7はリーデイングエツジ
パルス信号、8はトレーデイングエツジパルス信
号、10はデスピンモータアセンブリ、14はリ
フレクタ、15は衛星レーザピツクアツプ、16
はリードワイヤ、17は通信用アンテナ、18は
アンテナ位置パルス信号を示す。尚、各図中同一
符号は、同一又は相当部分を示す。
FIG. 1 shows the state in which the despin motor assembly of a spin-stabilized artificial satellite, which is an embodiment of this invention, is fixed to the satellite body, and the antenna position pulse signal output from the laser pickup.
The figure is a principle diagram showing a method of detecting an antenna pointing error using a conventional spin-stabilized artificial satellite, and FIG. 3 is a sectional view of a conventional despin motor assembly. In the figure, 1 is the earth, 2 is the despin part, 3 is the satellite body, 4 is the earth sensor, 7 is the leading edge pulse signal, 8 is the trading edge pulse signal, 10 is the despin motor assembly, 14 is the reflector, 15 is a satellite laser pick-up, 16
17 is a lead wire, 17 is a communication antenna, and 18 is an antenna position pulse signal. Note that the same reference numerals in each figure 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] 軌道上にて、衛星本体と反対方向に回転するデ
スピンモータアセンブリ、このモータのデスピン
部に取付けられている通信用アンテナとを備えた
スピン安定型人工衛星に於て、デスピンする通信
用アンテナの指向主軸上に取付けたリフレクタと
、衛星本体に取付けられ、レーザ光を発するとと
もに上記リフレクタからの反射光を検知し、アン
テナ位置パルス信号を発生するレーザピツクアツ
プとを備えたことを特徴とするスピン安定型人工
衛星。
In a spin-stabilized artificial satellite, which is equipped with a despin motor assembly that rotates in the opposite direction to the satellite body in orbit, and a communication antenna attached to the despin part of this motor, the communication antenna that despins. A spin stabilizer characterized by comprising a reflector mounted on the main directivity axis, and a laser pick-up mounted on the satellite body that emits a laser beam, detects the reflected light from the reflector, and generates an antenna position pulse signal. type artificial satellite.
JP12790888U 1988-09-29 1988-09-29 Pending JPH0249800U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP12790888U JPH0249800U (en) 1988-09-29 1988-09-29

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP12790888U JPH0249800U (en) 1988-09-29 1988-09-29

Publications (1)

Publication Number Publication Date
JPH0249800U true JPH0249800U (en) 1990-04-06

Family

ID=31380762

Family Applications (1)

Application Number Title Priority Date Filing Date
JP12790888U Pending JPH0249800U (en) 1988-09-29 1988-09-29

Country Status (1)

Country Link
JP (1) JPH0249800U (en)

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