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Spacecraft structure with symmetrical mass center and asymmetrical deployable appendages
Spacecraft structure with symmetrical mass center and asymmetrical deployable appendages
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机译:具有对称质心和不对称可展开附件的航天器结构
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摘要
An orbiting satellite system includes an asymmetrically deployed antenna and two deployable solar cell arrays. The solar cell arrays are deployed to a location which compensates for the asymmetry of the antenna so that the resulting station keeping thruster torques balance. Also, the system surfaces may be configured and the arrays so deployed to balance solar pressure torques on the system.
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