|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64G-001/10 B64G-001/28 B64G-001/26 B64G-001/40 B64G-001/24 B64G-001/44|
|미국특허분류(USC)||244/158.6; 244/168; 244/164|
|우선권정보||FR-11 02835 (2011-09-19)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 3 인용 특허 : 30|
A method of controlling the attitude of a satellite in orbit around a celestial body. The attitude of the satellite being controlled by a momentum storage device and controllable surfaces of the satellite configured to create desaturation torques in the storage device by using solar pressure. The controllable surfaces are arranged on solar panels mobile in rotation around an axis Y. At least one electric thruster configured to control the orbit of the satellite also controls the attitude of the satellite. The orientation of the electric thruster is contr...
1. A method of controlling an attitude of a satellite in orbit around a celestial body, comprising the steps of: controlling the attitude of the satellite by: an angular momentum storage device;controllable surfaces of the satellite configured to generate torques Cs for de-saturating the storage device by utilizing solar pressure, the controllable surfaces being arranged on mobile solar panels that rotates around a Y axis; andat least one electric thruster that also controls the orbit of the satellite;controlling an orientation of said at least one elect...