Research on Multi-Mode Control Strategy for Spaceborne Antenna Pointing Mechanism

Yuan Li, Zhijuan Liu, Huanqiang Chen, Chengshan Liu, Ke Zhu
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Abstract

The key problem of the spaceborne antenna pointing mechanism is to achieve high static pointing accuracy and realize fast dynamic tracking within the pointing range. In order to improve the static pointing and dynamic tracking accuracy, this paper utilizes a single-position closed-loop control algorithm to control the spaceborne antenna pointing mechanism, which works in the preset mode and tracking mode, meanwhile introduces feedforward control strategy. Finally, based on Matlab/Simulink, the simulation platform of the pointing control system is built to verify the control performance of the algorithm. The simulation results show that the steady-state error can reach 10-4° when kp=0.03, and the tracking accuracy can reach 10-4° after stabilization. This algorithm can satisfy the requirement of control error which should be less than 0.02°. Furthermore it can shorten the adjusting time with feedforward control strategy.
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星载天线指向机构多模态控制策略研究
星载天线指向机构的关键问题是在指向范围内实现高静态指向精度和快速动态跟踪。为了提高星载天线指向机构的静态指向和动态跟踪精度,采用单位置闭环控制算法对星载天线指向机构进行控制,使其工作在预置模式和跟踪模式下,同时引入前馈控制策略。最后,基于Matlab/Simulink搭建了指向控制系统仿真平台,验证了算法的控制性能。仿真结果表明,当kp=0.03时,系统的稳态误差可达10-4°,稳定后的跟踪精度可达10-4°。该算法能满足控制误差小于0.02°的要求。采用前馈控制策略可以缩短系统的调整时间。
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