A method of providing attitude and antenna steering for a spacecraft having a number of reaction wheels and a number of antennas is disclosed. The method includes determining a beta angle, the beta angle being the angle between a sun vector and an orbit plane of the spacecraft, and engaging either a...http://www.google.es/patents/US8123173?utm_source=gb-gplus-sharePatente US8123173 - Attitude and antenna steering system and method for spacecraft
Attitude and antenna steering system and method for spacecraft