6-DOF Formation Keeping Control for Three-Craft Electromagnetic Formation with Triangular Invariant Shape*

Huan Huang, Wei-wei Cai, Fudong Chu, Le-ping Yang
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引用次数: 0

Abstract

Spacecraft relative motion control with inter-craft electromagnetic force has distinct advantages, and its invariant shapes which are convenient for formation keeping ensure some significant potential applications. However, the electromagnetic actuators affect both the relative trajectory and attitude motion, complicating related studies on issues of invariant shape design and formation control. This paper mainly focuses on the formation keeping control for three-craft electromagnetic formation with triangular invariant shape on the basis of a 6-DOF full nonlinear dynamic model. Considering the high nonlinearity, strong coupling, model uncertainties and external disturbances, a combined control scheme involving feed-forward and feedback control components is proposed. The feed-forward component is obtained through desired invariant shape design which is complicated by the superposition and coupling effects of any two distinct magnetic dipoles. The feedback component is realized utilizing linear feedback controller based on the LQR method and active disturbance rejection control based on the extended state observer. Finally, the numerical simulation is presented to verify the feasibility and validity of the proposed 6-DOF control scheme.
三角不变形状三艇电磁编队六自由度保持控制*
利用航天器间电磁力进行航天器相对运动控制具有明显的优势,其形状的不变性便于编队保持,从而保证了航天器相对运动控制具有重要的应用前景。然而,电磁作动器既影响相对轨迹运动,又影响姿态运动,使不变形状设计和编队控制的相关研究变得复杂。本文主要研究基于六自由度全非线性动力学模型的三角不变形状三艇电磁编队保持控制问题。考虑到系统的高非线性、强耦合、模型不确定性和外部干扰,提出了一种前馈和反馈组合控制方案。前馈分量由任意两个不同磁偶极子的叠加和耦合效应所复杂的期望不变形状设计获得。利用基于LQR方法的线性反馈控制器和基于扩展状态观测器的自抗扰控制实现反馈分量。最后,通过数值仿真验证了所提出的六自由度控制方案的可行性和有效性。
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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