论文:2022,Vol:40,Issue(2):458-464
引用本文:
路阳, 蔡彬, 乔道鹏, 付艳明, 张卯瑞. 执行器跳变故障的失效卫星轨迹跟踪控制[J]. 西北工业大学学报
LU Yang, CAI Bin, QIAO Daopeng, FU Yanming, ZHANG Maorui. Trajectory tracking control of failure satellite with actuator jumping fault[J]. Northwestern polytechnical university

执行器跳变故障的失效卫星轨迹跟踪控制
路阳1,2, 蔡彬2, 乔道鹏2, 付艳明1, 张卯瑞1
1. 哈尔滨工业大学 控制理论与制导技术研究中心, 黑龙江 哈尔滨 150001;
2. 北京电子工程总体研究所, 北京 100854
摘要:
研究了执行器跳变故障的失效卫星轨迹跟踪控制问题,提出了具有跳变控制输入的模型参考跟踪控制器设计方法。结合随机稳定和模型参考跟踪定义,给出了失效卫星轨迹跟踪控制的问题描述。同时考虑系统存在扰动以及推力受限情形,利用线性矩阵不等式方法和非齐次广义Sylvester矩阵方程的参数化解方法,分别设计了对干扰具有抑制效果的鲁棒H状态反馈控制律和完全参数化形式的前馈补偿器。将所提出的方法应用于卫星在轨交会控制系统的控制器设计,仿真结果验证了所提方法的有效性。
关键词:    跳变故障    失效卫星    模型参考跟踪    参数化方法   
Trajectory tracking control of failure satellite with actuator jumping fault
LU Yang1,2, CAI Bin2, QIAO Daopeng2, FU Yanming1, ZHANG Maorui1
1. Center for Control Theory and Guidance Technology, Harbin Institute of Technology, Harbin 150001, China;
2. Beijing Institute of Electronic System Engineering, Beijing 100854, China
Abstract:
This paper studied the trajectory tracking control of a failure satellite that has actuator jumping fault. It proposed a design method based on the jumping control input for the model reference tracking controller. By comb-ining the stochastic stability definition with model reference tracking, it gave the mathematical descriptions of the trajectory tracking control of the failure satellite. It used the linear matrix inequality method and the parametric solution method of the nonhomogeneous generalized Sylvester matrix equation to design the robust H state feedback control law and the complete parametric feed-forward tracking compensator respectively, with the disturbance of the failure satellite and its thrust constraint considered simultaneously. The numerical simulation results on the model of the satellite rendezvous system show that the design method proposed in this paper is effective.
Key words:    actuator jumping fault    failure satellite    model reference tracking    parametric method    trajectory tracking control   
收稿日期: 2019-11-13     修回日期:
DOI: 10.1051/jnwpu/20224020458
通讯作者:     Email:
作者简介: 路阳(1987-),哈尔滨工业大学博士研究生,主要从事鲁棒控制、卫星姿态与轨道控制研究。e-mail:kongzhizidonghua@163.com
相关功能
PDF(1403KB) Free
打印本文
把本文推荐给朋友
作者相关文章
路阳  在本刊中的所有文章
蔡彬  在本刊中的所有文章
乔道鹏  在本刊中的所有文章
付艳明  在本刊中的所有文章
张卯瑞  在本刊中的所有文章

参考文献:
[1] 李新刚, 裴胜伟. 国外航天器在轨捕获技术综述[J]. 航天器工程, 2013, 22(1):113-119 LI Xingang, PEI Shengwei. On-orbit capture technology of spacecraft[J]. Spacecraft Engineering, 2013, 22(1):113-119 (in Chinese)
[2] 胡勇, 徐李佳, 解永春. 针对失控翻滚目标航天器的交会对接控制[J]. 宇航学报, 2015, 36(1):47-57 HU Yong, XU Lijia, XIE Yongchun. Control for rendezvous and docking with a tumbling target spacecraft[J]. Journal of Astronautics, 2015, 36(1):47-57 (in Chinese)
[3] ZHOU B, WANG Q, LIN Z L, et al. Gain scheduled control of linear systems subject to actuator saturation with application to spacecraft rendezvous[J]. IEEE Trans on Control Systems Technology, 2014, 22(5):2031-2038
[4] 姜博严, 胡庆雷, 石忠, 等. 与自由翻滚目标近距离段交会对接的相对姿轨耦合控制[J]. 宇航学报, 2014, 35(1):54-60 JIANG Boyan, HU Qinglei, SHI Zhong, et al. Relative position and attitude coupled controller design for approaching and docking with a freely tumbling target[J]. Journal of Astronautics, 2014, 35(1):54-60 (in Chinese)
[5] 邓泓, 孙兆伟, 仲惟超. 控制输入受限的拦截卫星轨道鲁棒H2/H控制[J]. 控制理论与应用, 2012, 29(9):1108-1114 DENG Hong, SUN Zhaowei, ZHONG Weichao. Robust H2/H orbit control for intercepting spacecraft with control input constraint[J]. Control Theory and Applications, 2012, 29(9):1108-1114 (in Chinese)
[6] EPENOY R. Fuel optimization for continuous-thrust orbital rendezvous with collision avoidance constraint[J]. Journal of Guidance, Control, and Dynamics, 2011, 34(2):493-503
[7] AHSUN U, MILLER D W, RAMIRES J L. Control of electromagnetic satellite formations in near earth orbits[J]. Journal of Guidance, Control, and Dynamics, 2010, 33(6):1183-1891
[8] PETERS T V, NOOMEN R, COLMENAREJO P. Analytical solutions to two-impulse nondrifting transfer problems for rendez-vous in elliptical orbits[J]. Journal of Guidance, Control, and Dynamics, 2014,37(3):775-788
[9] 付艳明, 李伟, 段广仁. 基于T-H方程的卫星轨迹模型参考输出跟踪控制方法[J]. 宇航学报, 2013, 34(4):496-502 FU Yanming, LI Wei, DUAN Guangren. Satellite trajectory model reference output tracking control based on T-H equation[J]. Journal of Astronautics, 2013, 34(4):496-502 (in Chinese)
[10] ZHENG G W, DONG S L, SHI P, et al. Fuzzy-model-based nonfragile guaranteed cost control of nonlinear markov jump systems[J]. IEEE Trans on Systems, Man, and Cybernetics:Systems, 2017, 47(8):2388-2397
[11] MA H J, JIA Y M. H2 control of discrete-time periodic systems with markovian jumps and multiplicative noise[J]. International Journal of Control, 2013, 86(10):1837-1849
[12] FRAGOSO M D, BACZYNSKI J. Lyapunov coupled equations for continuous-time infinite Markov jump linear systems[J]. Journal of Mathematical Analysis and Applications, 2002, 274(1):319-335
[13] BOUKAS E K. On reference model tracking for Markov jump systems[J]. International Journal of Systems Science, 2009, 40(4):393-401
[14] BOUKAS E K. H control of discrete-time markov jump systems with bounded transition probabilities[J]. Optimal Control Applications and Methods, 2009, 30(1):477-494
[15] YANG H J, Li H B, SUN F C, et al. Robust control for Markovian jump delta operator systems with actuator saturation[J]. European Journal of Control, 2014, 20(4):207-215
[16] FU Y M, LU Y, ZHANG M R. Model reference tracking control of continuous-time periodic linear systems with actuator jumping fault and applications in orbit maneuvering[J]. International Journal of Control, Automation and Systems, 2017, 15(5):2182-2192