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The configuration of the artificial satellite attitude control allowing a continuous along three axes
The configuration of the artificial satellite attitude control allowing a continuous along three axes
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机译:人造卫星姿态控制的配置允许沿三个轴连续
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摘要
A spacecraft configuration including a service module which carries optical stabilizing equipment for stabilizing the spacecraft relative to two inertially fixed targets together with solar arrays rigidly attached thereto so as to extend in the orbital plane and never obstruct the field of view of the optical stabilization equipment. The payload module is attached to one face of the service module by means of rotary interface structure to be able to continuously point to the earth.
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