发明名称 |
Spacecraft attitude control system using low thrust thrusters |
摘要 |
A spacecraft, such as a geosynchronous weather or communications satellite, is constructed to include a plurality of low thrust thrusters mounted at predetermined locations on at least one of a spacecraft appendage or a spacecraft bus. The plurality of low thrust thrusters are fired in pairs for at least one of removing a disturbance torque or providing fine pointing attitude control. In one embodiment the low thrust thrusters are mounted on a solar array panel, thereby increasing the moment arm and enhancing the thrust output of the low thrust thrusters. In one embodiment a spacecraft has a plurality of low thrust thrusters arranged as at least two sets of two low thrust thrusters, individual ones of the low thrust thrusters of a set being disposed in a V-configuration and mounted at predetermined locations on at least one of a spacecraft appendage or a spacecraft bus. The plurality of low thrust thrusters are selectively fired for achieving control of 3-axes of spacecraft attitude or momentum.
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申请公布号 |
US6053455(A) |
申请公布日期 |
2000.04.25 |
申请号 |
US19980010718 |
申请日期 |
1998.01.22 |
申请人 |
SPACE SYSTEMS/LORAL, INC. |
发明人 |
PRICE, XEN;RANDOLPH, THOMAS;CHAN, KAM K.;KAMEL, AHMED |
分类号 |
B64G1/26;B64G1/28;B64G1/36;(IPC1-7):B64G1/26 |
主分类号 |
B64G1/26 |
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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