发明名称 |
Dynamic bias for orbital yaw steering |
摘要 |
<p>A method and apparatus for steering a low-earth-orbit communication satellite requiring sun-orientation for solar-power accumulation is disclosed. Momentum-bias both maintains nadir pointing and adds yaw-steering moments for sun-tracking attitude control, simultaneously. The method has two principal steps: 1) open-loop momentum decoupling, for correcting the calculated steering torque, and closed-loop attitude compensation, to correct for perturbations about the calculated attitude in accordance with one of two control law definitions. This combines the advantage of stable gyroscopic attitude control with those of open-loop yaw steering. <IMAGE></p> |
申请公布号 |
EP0785132(A1) |
申请公布日期 |
1997.07.23 |
申请号 |
EP19970300076 |
申请日期 |
1997.01.08 |
申请人 |
GLOBALSTAR L.P.;DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT |
发明人 |
RODDEN, JOHN J.;FICHTER, WALTER;FURUMOTO, NOBUO;BRUEDERLE, ERNST |
分类号 |
G01C21/24;B64G1/28;B64G1/36;G05D1/08;(IPC1-7):B64G1/36 |
主分类号 |
G01C21/24 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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