The invention relates to the field of spaceflight satellites, in particular to a satellite in-orbit operation method, a satellite orbital transfer method and a rotating satellite. The satellite in-orbit operation method comprises the steps that first height information of an orbit satellite at the orbit height of 35786 km is obtained, first surrounding speed information of the first height information is obtained, and the surrounding speed information is first length information; second height information of an orbit where the rotating satellite is located is obtained, and second surrounding speed information corresponding to the second height information is obtained according to the second height information; the second surrounding speed information is second length information; obtaining first difference length information by using the first length information and the second length information; acquiring perimeter information of the rotating satellite rotating for one circle; obtaining first rotation information of the rotating satellite according to the first difference length information and the perimeter information; keeping the rotating satellite in a self-rotating state at a first rotating speed in an orbit; the rotating speed of the first rotating speed is second rotating information.
本发明涉及航天卫星领域,具体为卫星在轨运行方法及卫星变轨方法和旋转卫星。本发明卫星在轨运行方法,包括:轨道卫星在轨道高度35786km为第一高度信息,获得所述第一高度信息的第一环绕速度信息,该环绕速度信息为第一长度信息;获取旋转卫星所处轨道的第二高度信息,并根据所述第二高度信息获得与之对应的第二环绕速度信息;该第二环绕速度信息为第二长度信息;利用所述第一长度信息和所述第二长度信息得出第一差异长度信息;获取所述旋转卫星旋转一圈的周长信息;并根据所述第一差异长度信息和所述周长信息得出所述旋转卫星的第一旋转信息;将所述旋转卫星在轨道以第一转速保持自身旋转状态;该第一转速的转速为第二旋转信息。
Satellite in-orbit operation method, satellite orbital transfer method and rotating satellite
卫星在轨运行方法及卫星变轨方法和旋转卫星
2025-01-07
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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