基于反步法的空间目标复合指向控制方法研究

doi:10.12305/j.issn.1001-506X.2023.09.28

Abstract

Abstract:

A composite platform high precision control method composed of satellite platform and two-dimensional turntable is proposed for space moving target high precision attitude tracking. Firstly, the coupled dynamics model of the composite platform is established. Secondly, the backstepping controller is designed for the satellite to achieve coarse tracking. When the attitude error meets certain switching requirement, the two-dimensional turntable adopts the model predictive controller based on the loading observer to assist the satellite to perform the attitude precision tracking. In addition, the nonlinear disturbance observer is designed to estimate the disturbance torque generated by the coupled motion on the satellite body. Finally, the numerical simulation results show that the attitude accuracy of the proposed method can be improved by an order of magnitude, which can realize high-precision attitude tracking control, and provide research basis for engineering practice.

Key words: space moving target, dynamic tracking, composite platform, coupled dynamics, model predictive control

CLC Number:

V448.22+2

Hong ZHANG, Yunhua WU, Shengjun ZHONG, Haibo GUO. Space target compound pointing control method based on backstepping[J]. Systems Engineering and Electronics, 2023, 45(9): 2884-2893.

Figures/Tables 20

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参数	取值
俯仰轴转动惯量J_py/kg·m²	0.08
方位轴转动惯量J_pz/kg·m²	0.05
方位部分质量m₁/kg	10
俯仰部分质量m₂/kg	5
电机转动惯量J_m/kg·m²	0.03
电机磁极对数p_n	5
电阻R/Ω	0.369
电感L/mH	2.4
摩擦系数B/(N·m·s/rad)	0.004 7
转台测量误差/(°)	0.000 01
转台干扰力矩/N·m	10^-5

姿态算法	反步法+模型预测	PD+迭代学习	反步法+PID
姿态跟踪误差/(°)	0.5×10^-4	0.005	0.004
姿态角速度/(°/s)	0.001	0.02	0.01
开始收敛时间/s	30	50	35
是否需要迭代	否	是	否

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Space target compound pointing control method based on backstepping

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