The invention provides a satellite locking method and device and a computer readable storage medium. The locking method comprises the following steps of acquiring a first satellite alignment angle and a second satellite alignment angle of a satellite antenna, the first satellite alignment angle being asatellite alignment angle under a geographic coordinate system, and the second satellite alignment angle being a theoretical satellite alignment angle, controlling the satellite antenna to rotate to a second satellite alignment angle, obtaining the maximum value of the beacon signal strength of the satellite antenna in a preset range, and taking the maximum value of the beacon signal strength as a target position of the satellite antenna, and controlling the satellite antenna to rotate to the target position, so that the to-be-locked satellite is locked through the method, and the satellite can be quickly and accurately locked.
本发明提供了一种卫星的锁定方法及设备、计算机可读存储介质。锁定方法包括:获取卫星天线的第一对星角及第二对星角,第一对星角为地理坐标系下的对星角,第二对星角为理论对星角;控制卫星天线转动至第二对星角;获取卫星天线在预设范围内信标信号强度的最大值,并将信标信号强度的最大值处作为卫星天线的目标位置;控制卫星天线转动至目标位置处,从而实现对待锁定卫星的锁定通过上述方法,本发明能够快速准确的锁定卫星。
Satellite locking method and device, and computer readable storage medium
一种卫星的锁定方法及设备、计算机可读存储介质
2021-06-18
Patent
Elektronische Ressource
Chinesisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
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