发明名称 |
Method and apparatus for rate integration supplement for attitude referencing with quaternion differencing |
摘要 |
A control system for providing attitude control in spacecraft. The control system comprising a primary attitude reference system, a secondary attitude reference system, and a hyper-complex number differencing system. The hyper-complex number differencing system is connectable to the primary attitude reference system and the secondary attitude reference system.
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申请公布号 |
US6454217(B1) |
申请公布日期 |
2002.09.24 |
申请号 |
US20000670904 |
申请日期 |
2000.09.28 |
申请人 |
SPACE SYSTEMS/LORAL, INC. |
发明人 |
RODDEN JOHN JAMES;PRICE XENOPHON;CARROU STEPHANE;STEVENS HOMER DARLING |
分类号 |
B64G1/24;B64G1/26;B64G1/28;B64G1/36;G05D1/08;(IPC1-7):B64G1/24 |
主分类号 |
B64G1/24 |
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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