Method for generating safe-mode attitude command of satellite at failure in solar-array drive assembly

Method for generating safe-mode attitude command of satellite at failure in solar-array drive assembly

The present invention relates to a method for generating a safety mode attitude command of a satellite when a solar panel driver fails. The present invention is to provide a method for generating a safety mode attitude command of a satellite when a solar panel driver fails, which enables smooth powe...

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Hauptverfasser: PARK JOOHO, BAEK KWANGYUL, AHN HANWOONG
Format: Patent
Sprache:eng ; kor
Schlagworte:
AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
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creator PARK JOOHO
BAEK KWANGYUL
AHN HANWOONG
description The present invention relates to a method for generating a safety mode attitude command of a satellite when a solar panel driver fails. The present invention is to provide a method for generating a safety mode attitude command of a satellite when a solar panel driver fails, which enables smooth power supply and demand when operating in safe mode by ensuring that the solar panel correctly points the sun even if the solar panel driver is broken when entering the safe mode in the satellite. 본 발명은 태양전지판 구동기 고장 시 인공위성의 안전모드 자세명령 생성방법에 관한 것이다. 본 발명의 목적은, 인공위성에서 안전모드로 돌입할 때 태양전지판 구동기가 고장난 상태라 하더라도 태양전지판이 올바르게 태양을 지향할 수 있도록 함으로써 안전모드 운용 시 전력수급이 원활하게 이루어질 수 있도록 해 주는, 태양전지판 구동기 고장 시 인공위성의 안전모드 자세명령 생성방법을 제공함에 있다.
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subjects AIRCRAFT
AVIATION
COSMONAUTICS
PERFORMING OPERATIONS
TRANSPORTING
VEHICLES OR EQUIPMENT THEREFOR
title Method for generating safe-mode attitude command of satellite at failure in solar-array drive assembly
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