The invention relates to a high-orbit satellite orbital transfer regulation and control method and system, and the method comprises the steps: determining a to-be-executed orbital maneuvering mode of a high-orbit satellite in advance through the high-orbit satellite orbital transfer regulation and control system; acquiring orbital transfer regulation and control parameters for transferring the high-orbit satellite from an initial orbit to a target orbit by using a preset orbital transfer regulation and control relational expression; and performing orbital transfer regulation and control on the high-orbit satellite by using the orbital transfer regulation and control parameters, and regulating and controlling the high-orbit satellite from an initial position on the initial orbit to an expected position where a relative position with a target satellite meets the orbital maneuvering mode. According to the technical scheme provided by the invention, the inventor puts forward the orbital transfer regulation and control relational expression based on own research, and obtains and utilizes the orbital transfer regulation and control parameters based on the orbital transfer regulation and control relational expression to realize orbital transfer regulation and control of the high-orbit satellite in the predetermined orbit maneuvering mode.
本发明涉及一种高轨卫星变轨调控方法及系统,本发明中,高轨卫星变轨调控系统预先确定高轨卫星待执行的轨道机动模式;利用预设变轨调控关系式,获取用于将所述高轨卫星从初始轨道变轨到目标轨道的变轨调控参数;利用所述变轨调控参数对所述高轨卫星进行变轨调控,将所述高轨卫星从所述初始轨道上初始位置,调控至与目标卫星之间的相对位置满足所述轨道机动模式的预期位置。本发明提供的技术方案,发明人基于自己的研究,提出变轨调控关系式,基于变轨调控关系式,获取并利用变轨调控参数,来实现预定轨道机动模式下,高轨卫星的变轨调控。
High-orbit satellite orbital transfer regulation and control method and system
一种高轨卫星变轨调控方法及系统
2022-05-27
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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