专利内容由知识产权出版社提供
专利名称：METHOD FOR CONTROLLING THE
GUIDANCE OF ATTITUDE OF A SATELLITE,SATELLITE, PLURALITIES OF SATELLITES,AND ASSOCIATED COMPUTER PROGRAMME
发明人：GIRAUD, Emmanuel申请号：EP17708861.4申请日：20170213公开号：EP3390230B1公开日：20190612
摘要：The invention relates to a method for controlling the guidance of attitude of asatellite (1), the satellite comprising an optical instrument (2), and a solar generator (4)defining a functional surface. The method comprises a first step of transmission (104) ofguidance control for pointing the sighting axis (V) of the optical instrument in thedirection of regions (7) to be imaged and a second step of transmission (106) of guidancecontrol for orienting the normal (N, Na, Nb) towards the functional surface in thedirection of the solar radiation. The guidance controls only relate to the rotation of thesatellite about the speed axis (X), the angle of rotation about the orbit axis (Y) and thenadir axis (Z) in the orbital reference frame being maintained at substantially zero.
申请人：Airbus Defence and Space SAS,AIRBUS DEFENCE & SPACE SAS,AIRBUSDEFENCE AND SPACE SAS
地址：FR
国籍：FR
代理机构：Cabinet Plasseraud
更多信息请下载全文后查看
