发明名称 |
ATTITUDE CONTROL FOR AGILE SATELLITE APPLICATIONS |
摘要 |
The present invention relates to attitude control and, in particular, to control of the attitude of a space platform. The space platform may take the form of or be part of a satellite and/or a spacecraft. An aspect of the present invention concerns the use, in an attitude control system, of several control moment gyroscopes with limited gimbal revolutions. Another aspect of the present invention concerns an improved logic for controlling a control moment gyroscope assembly of an attitude control system. |
申请公布号 |
SG11201604913T(A) |
申请公布日期 |
2016.07.28 |
申请号 |
SGT11201604913 |
申请日期 |
2014.12.23 |
申请人 |
THALES ALENIA SPACE ITALIA S.P.A. CON UNICO SOCIO |
发明人 |
ANANIA, MARCO;CASCONE, DOMENICO |
分类号 |
B64G1/28;G01C19/00;G05D1/08 |
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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