|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||244/168 ; 244/173|
|§371/§102 date||19920724 (19920724)|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 21 인용 특허 : 0|
A satellite embodying at least one surface intended mainly for exposure to solar radiation and extending away from the satellite in a predetermined direction (Y), an on-board computer having connected thereto an attitude sensing system, an orbit control system for imparting thrust to the satellite along predetermined axes, and an attitude control system. The satellite further embodies a device for controlling the tilt of the surface in parallel with a plurality of planes containing the predetermined direction; and, therefore, particularly in parallel wit...
An attitude control system for a satellite, said attitude control system comprising: a satellite having attitude stabilizing means for controlling said attitude about a pitch, yaw and roll axis while said satellite is in a geostationary orbit; an onboard computer mounted to said satellite, said attitude stabilizing means being in communication with said onboard computer; at least one surface member extending from said satellite in a first direction away from said satellite, said at least one surface member adapted to be exposed to solar radiation; orbit ...