空间变轨过程中的跨尺度滤波与控制研究

段广仁

摘要：本年度主要针对空间变轨过程中的跨尺度滤波与控制方法，基于前期理论研究成果，围绕航天飞行器的鲁棒控制基础理论、航天器鲁棒姿轨联合控制、航天器编队飞行协同控制、基于非线性滤波的卫星运动估计、航天器鲁棒容错控制，航天器的鲁棒轨道控制及航天器的鲁棒姿态控制等七个方面展开了研究，取得了相关研究成果。 鲁棒控制基础理论部分主要针对具有状态和输入时滞的线性系统的镇定问题，输入和输出具有时滞的控制系统的观测器设计，时变线性系统的镇定Lyapunov微分方程方法，具有输入时滞线性系统的高阶截断预估器反馈方法，控制受限连续时间周期系统的L∞及L2半全局镇定，状态受限线性系统的滤波器设计，Sylvester方程的显示解及共轭代数Lyapunov方程的有限迭代求解算法及具有不确定性时滞系统的稳定性判据等八个方面取得的理论研究成果进行了详细阐述。 航天器鲁棒姿轨联合控制部分总结了近圆轨道目标交会的航天器鲁棒姿轨联合控制及应用于空间拦截任务中的航天器鲁棒姿轨联合控制的相关研究成果。 航天器编队飞行协同控制部分给出了编队飞行航天器六自由度鲁棒协同控制的研究成果。 基于非线性滤波的卫星运动估计部分总结了基于改进容积卡尔曼滤波的卫星姿态估计相关研究成果。 航天器鲁棒容错控制及航天器的鲁棒轨道控制部分针对基于特征结构配置的鲁棒容错控制及非线性系统的鲁棒自适应故障诊断控制进行了概述。 航天器的鲁棒轨道控制部分针对航天器轨道交会的全局镇定及航天器轨迹模型参考输出跟踪控制方法等两个方面的研究成果进行了总结。 最后总结了航天器的鲁棒姿态控制的相关研究结果。

关键词：航天器控制；滤波；鲁棒控制；容错控制；协同控制

The Report of the Multi-Scale Filtering and Control for Spacecraft Orbital Transfer

Abstract：The report presents the research background， significance and basic theory， and summarizes the study results this year. Based on former results， we study around the seven aspects： the robust control basic theory of the spacecraft， the robust integrated translational and rotational control for spacecraft， the cooperative control for spacecraft formation flying， the motion estimation of spacecraft based on the nonlinear filtering， the robust fault-tolerant control for spacecraft， the robust orbital control for spacecraft and the robust attitude control of spacecraft. In the section of robust control basic theory， we summarized the results on the stabilization of the linear system with input delay and state delay， stabilization of time-varying linear systems via Lyapunov differential equations， the higher-order truncated predictor feedback for linear systems with input delay， L∞ and L2 semi-global stabilization of continuous time periodic linear systems with bounded controls， some results on the constrained state filtering， explicit solutions to one class of Sylvester equation， etc. Some results on the robust integrated translational and rotational control for spacecraft rendezvous and space interception are summarized in the section of the robust integrated translational and rotational control for spacecraft. The results on 6-DOF robust cooperative control for the spacecraft formation flying are given in the section of the cooperative control for spacecraft formation flying. The section of the motion estimation of spacecraft based on the nonlinear filtering summarizes the results on the estimation of spacecraft attitude based on the improved volume Kalman filtering. The results on robust fault-tolerant control based on eigenstructure assignment and robust actuator fault diagnosis scheme for satellite attitude control systems are summarized in the section of the robust fault-tolerant control for spacecraft. The results on the global stabilization control for spacecraft orbital rendezvous system and the model reference output tracking control for spacecraft are prescribed in the section of robust orbital control for spacecraft. Finally， we summarize the related results on the robust attitude control of spacecraft. The report lists some semi-physical simulations to illustrate the effectiveness and practicability of the obtained results

Keywords：Space control； filtering； robust control； fault-tolerant control； cooperative control

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