发明名称 |
System for controlling the direction of the momentum vector of a geosynchronous satellite |
摘要 |
A system for compensating the disturbance torques applied to a satellite, which eliminates the requirement for a thruster control loop. The disturbance torque itself is used as the compensating torque in order to super-impose to the incidental misalignment of the solar panel arrays an artificial misalignment that can cause the momentum vector to be adjusted to the desired direction in order to restore the correct attitude of the satellite. The direction of the momentum vector is controlled in orbit only by solar sailing, that is by organizing at prescribed times suitable manoeuvres of one of the solar panels in order to adjust the solar panel array configuration when the roll angle of the satellite exceeds a determined threshold value.
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申请公布号 |
US4325124(A) |
申请公布日期 |
1982.04.13 |
申请号 |
US19800118847 |
申请日期 |
1980.02.05 |
申请人 |
ORGANISATION EUROPEENNE DE RECHERCHES SPATIALES |
发明人 |
RENNER, UDO |
分类号 |
B64G1/24;B64G1/36;B64G1/40;B64G1/44;G01S3/78;G05D1/08;(IPC1-7):G06F15/50 |
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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