The invention discloses a spin nutation coupling racemization plume pointing method and system based on plume racemization, and belongs to the technical field of spacecrafts, and the method comprises the steps: collecting the rotational inertia and angular velocity data of a target in a motion state; counting spinning-nutation racemization torque parameters capable of being received by the target solar panel in the racemization process; inputting the spin-nutation racemization torque parameter, the rotational inertia and the angular velocity data into a coupling racemization plume pointing model to obtain an optimal plume pointing point; and inputting the optimal plume pointing point into the plume racemization kinetic model for racemization calculation to obtain a racemization termination condition, and if the motion state of the target meets the racemization termination condition, completing the racemization task. According to the method, spin nutation coupling racemization of the target can be achieved according to the motion characteristic, the quality characteristic and the shape characteristic of the target, the problem that the racemization guidance law is insufficient is solved, and the method is suitable for various racemization modes in which a failure satellite solar panel is used for generating resistance torque.
本发明公开了一种基于羽流消旋的自旋章动耦合消旋羽流指向方法及系统,属于航天器技术领域,方法包括采集目标的运动状态中的转动惯量及角速度数据;统计消旋过程中目标太阳帆板能够收到的自旋‑章动消旋力矩参数;将自旋‑章动消旋力矩参数、转动惯量及角速度数据输入进耦合消旋羽流指向模型,获取最优羽流指向点;将最优羽流指向点输入进羽流消旋动力学模型中进行消旋计算获得消旋终止条件,若目标的运动状态满足消旋终止条件,则消旋任务完成。本发明能够根据目标的运动特性、质量特性以及形状特性,实现目标的自旋章动耦合消旋,解决消旋制导律不足的情况,且该方法适用于多种使用失效卫星太阳帆板产生阻力矩的消旋方式。
Spin nutation coupling racemization plume pointing method and system based on plume racemization
基于羽流消旋的自旋章动耦合消旋羽流指向方法及系统
2023-12-08
Patent
Electronic Resource
Chinese
IPC: | B64G Raumfahrt , COSMONAUTICS |
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