发明名称 |
Satellite attitude control system and method |
摘要 |
A satellite attitude control system includes a programmed processor system which includes a gyroscopic actuator first control stage for changing the attitude of the satellite and a reaction wheel second control stage for assuring that pointing of the satellite is accurate and stable. The method is intended to be used for a satellite including the two control stages indicated above, which it uses selectively for the operations indicated above.
|
申请公布号 |
US6499699(B1) |
申请公布日期 |
2002.12.31 |
申请号 |
US20000607956 |
申请日期 |
2000.06.30 |
申请人 |
ALCATEL |
发明人 |
SALENC CEDRIC;ROSER XAVIER |
分类号 |
B64G1/28;G05D1/08;(IPC1-7):B64G1/26 |
主分类号 |
B64G1/28 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|