The invention relates to a flywheel configuration and high-torque flywheel access and exit method and device for satellite rapid side-sway maneuver, computer equipment and a storage medium. In order to improve the maneuvering capability of rapid side-sway (namely rotating around the X axis of the satellite) of the satellite, a flywheel heterogeneous configuration for rapid side-sway maneuvering of the satellite is established; a high-torque flywheel access strategy is determined according to the flywheel heterogeneous configuration; and a high-torque flywheel exit strategy is determined according to the flywheel heterogeneous configuration. The heterogeneous flywheel is simple in structure, easy to implement and low in cost, and the rapid maneuvering capability of the optical satellite in the side-sway direction is remarkably improved. The access and exit strategy of the high-torque flywheel is simple and clear, and engineering realization is easy.
本发明是一种用于卫星快速侧摆机动的飞轮构型与大力矩飞轮接入退出方法、装置、计算机设备和存储介质。本发明为了提高卫星快速侧摆(即绕卫星X轴转动)机动能力,本发明建立用于卫星快速侧摆机动的飞轮异构构型;根据飞轮异构构型,确定大力矩飞轮接入策略;根据飞轮异构构型,确定大力矩飞轮退出策略。本发明采用的异构飞轮构型简单、易实现、成本低,对于光学卫星侧摆方向快速机动能力提升显著。大力矩飞轮接入退出策略简洁、清晰易于工程实现。
Flywheel configuration and high-torque flywheel access and exit method and device for satellite rapid side-sway maneuver, computer equipment and storage medium
一种用于卫星快速侧摆机动的飞轮构型与大力矩飞轮接入退出方法、装置、计算机设备和存储介质
2022-01-07
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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