发明名称 |
Integrated inertial stellar attitude sensor |
摘要 |
An integrated inertial stellar attitude sensor for an aerospace vehicle includes a star camera system, a gyroscope system, a controller system for synchronously integrating an output of said star camera system and an output of said gyroscope system into a stream of data, and a flight computer responsive to said stream of data for determining from the star camera system output and the gyroscope system output the attitude of the aerospace vehicle.
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申请公布号 |
US2004098178(A1) |
申请公布日期 |
2004.05.20 |
申请号 |
US20030621097 |
申请日期 |
2003.07.16 |
申请人 |
BRADY TYE M.;KOUREPENIS ANTHONY S.;WYMAN WILLIAM F. |
发明人 |
BRADY TYE M.;KOUREPENIS ANTHONY S.;WYMAN WILLIAM F. |
分类号 |
B64G1/28;B64G1/36;G01C21/02;G01C21/16;(IPC1-7):G06F17/00 |
主分类号 |
B64G1/28 |
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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