发明名称 METHOD FOR CONTROLLING THE ATTITUDE OF A SPINNING BODY IN ORBIT
摘要 METHOD FOR CONTROLLING THE ATTITUDE OF A SPINNING BODY IN ORBIT A method for passively stabilizing the attitude of a spinning orbiting body subject to orbital precession to maintain the spin axis orientation of the body essentially fixed and stable relative to the orbital plane. The preferred embodiment comprises selecting a body mass geometry and orbital parameters, including an orbit inclination, an orbital rate and a rate of regression of orbit line of nodes, so that the precessional motion of the body and the orbit are equal and opposite in direction and locating the spin axis of the body in a plane containing the north axis of the body and the orbit normal and between the north axis and the orbit normal, so that the gravity gradient precession of the spin axis equals the regressional motion of the orbit normal to produce a planar equilibrium configuration.
申请公布号 CA1287029(C) 申请公布日期 1991.07.30
申请号 CA19870539476 申请日期 1987.06.11
申请人 HUGHES AIRCRAFT COMPANY 发明人 MCINTYRE, JOHN E.
分类号 B64G1/24;B64G1/28;G05D1/08 主分类号 B64G1/24
代理机构 代理人
主权项
地址