Attitude control of ultra-low orbit satellite based on RBF neural network

Cai-zhi Fan, Shaoting Yu, Mengmeng Wang
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引用次数: 0

Abstract

Ultra-low-orbit satellites have the advantages of high resolution, high efficiency and low launch costs; however, atmospheric drag may lead to complex external interference, and continuous orbital fuel consumption may cause uncertain satellite rotation inertia. In view of the attitude control problem of ultra-low orbit satellite, this paper puts forward an adaptive attitude control method based on RBF neural network, which approaches the ideal slip mode controller through RBF neural network and adjusts neural network parameters according to external disturbance adaptation. The paper is designed to prove the progressive stability of the controller by Lyapunov theory and carried out the simulation verification. The simulation results show that the designed attitude controller can effectively overcome the influence of uncertainty disturbance in the system and improve the accuracy of attitude control.
基于RBF神经网络的超低轨道卫星姿态控制
超低轨道卫星具有分辨率高、效率高、发射成本低等优点;然而,大气阻力可能导致复杂的外部干扰,持续的轨道燃料消耗可能导致不确定的卫星旋转惯性。针对超低轨道卫星的姿态控制问题,提出了一种基于RBF神经网络的自适应姿态控制方法,该方法通过RBF神经网络逼近理想的滑模控制器,并根据外部扰动自适应调节神经网络参数。本文利用李雅普诺夫理论证明了控制器的渐进稳定性,并进行了仿真验证。仿真结果表明,所设计的姿态控制器能有效克服系统中不确定性干扰的影响,提高姿态控制精度。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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