发明名称 |
A method and apparatus for rate integration supplement for attitude referencing with quaternion differencing |
摘要 |
<p>A control system for providing attitude control in spacecraft. The control system comprises a primary attitude reference system (21), a secondary attitude reference system (22), and a hyper-complex number differencing system (23). The hyper-complex number differencing system is connectable to the primary attitude reference system and the secondary attitude reference system. <IMAGE></p> |
申请公布号 |
EP1193176(A2) |
申请公布日期 |
2002.04.03 |
申请号 |
EP20010308279 |
申请日期 |
2001.09.27 |
申请人 |
SPACE SYSTEMS / LORAL, INC. |
发明人 |
RODDEN, JOHN JAMES;CARROU, STEPHANE;PRICE, XENOPHON;STEVENS, HOMER DARLING |
分类号 |
G05D1/08;B64G1/24;B64G1/26;B64G1/28;B64G1/36;(IPC1-7):B64G1/24 |
主分类号 |
G05D1/08 |
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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