Solar torque estimation for momentum bias spacecraft

被引：0
|
作者：
McGovern, Lawrence K. [1 ]
Hirschberg, Philip [2 ]
Price, Xenophon [2 ]
机构：
[1] Lockheed Martin Space Systems Company, Sunnyvale, CA
[2] Space Systems/Loral, Palo Alto, CA
来源：
Journal of the Astronautical Sciences | 1600年 / 55卷 / 02期
关键词：
This paper introduces a solar torque estimation algorithm for momentum bias satellites; ultimately benefiting yaw pointing performance and momentum management. A subspace of the solar torque is demonstrated to be unobservable without the use of a rate sensor. By decomposing the solar torque environment into observable and unobservable components; this algorithm may be implemented with or without a rate-sensing gyro. Flight data are presented; sharing recent flight experiences with the algorithm in this paper. This telemetry is derived from several recent; large geosynchronous orbit (GEO) satellites; including one with a 12-meter deployable antenna;
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摘要：
Conference article (CA)
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页码：215 / 235
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