Polymerization type on-orbit structure-varying micro-nano satellite turn control method
A technology of micro-nano satellite and flip control, which is applied in the direction of space navigation vehicle guidance device, space navigation equipment, space navigation aircraft, etc. To solve problems such as limited ability to change the shape and configuration, to achieve the effect of convenient connection and separation, low cost, and powerful service
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[0034] Below in conjunction with accompanying drawing and specific embodiment the present invention is described in further detail:
[0035] The present invention provides a flip control method for aggregated on-orbit variable configuration micro-nano satellites, fully utilizes the advantages of compact and flexible micro-nano satellite modules, deeply explores and proposes a "polymeric on-orbit variable configuration micro-nano satellite system" The concept of innovative space system, "aggregated on-orbit variable configuration micro-nano satellite system" has high flexibility and scalability, and the components can be changed more conveniently, which can well meet the requirements of flexibility, high Dynamic disaster reduction remote sensing applications, large-scale space-based system construction and on-orbit maintenance service applications and other requirements.
[0036] Such as figure 1 The flow chart of module satellite flipping control is shown, and it can be seen ...
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