The invention discloses an orbit control method and device for a geosynchronous orbit communication satellite. The method comprises the following steps: determining a first control moment and a first control quantity of north-south maneuver, and controlling an orbit inclination angle according to the first control moment and the first control quantity; determining a second control moment and a second control quantity of east-west maneuvering, and controlling the satellite flat longitude according to the second control moment and the second control quantity; and determining a third control moment and a third control quantity of the double-pulse maneuver, and controlling the orbit eccentricity rate according to the third control moment and the third control quantity. The technical problems that in the prior art, orbit control operation risks are large, personnel and equipment pressure is large, and satellite fuel consumption is large are solved.
本申请公开了一种地球同步轨道通信卫星的轨道控制方法及装置,该方法包括:确定南北机动的第一控制时刻以及第一控制量,根据所述第一控制时刻以及所述第一控制量控制轨道倾角;确定东西机动的第二控制时刻以及第二控制量,根据所述第二控制时刻以及所述第二控制量控制卫星平经度;确定双脉冲机动的第三控制时刻以及第三控制量,根据所述三控制时刻以及所述第三控制量控制轨道偏心率。本申请解决了现有技术中轨道控制操控风险较大、人员设备压力大以及卫星燃料消耗较多的技术问题。
Orbit control method and device for geosynchronous orbit communication satellite
一种地球同步轨道通信卫星的轨道控制方法及装置
2021-07-30
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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