考虑避障的航天器编队轨道容错控制律设计

doi:10.7527/S1000-6893.2017.321129

电子电气工程与控制

本期目录 | 过刊浏览 | 高级检索

前一篇 | 后一篇

考虑避障的航天器编队轨道容错控制律设计

马广富¹, 董宏洋¹, 胡庆雷²

1. 哈尔滨工业大学航天学院, 哈尔滨 150001;
2. 北京航空航天大学自动化科学与电气工程学院, 北京 100083

收稿日期:2017-01-13 修回日期:2017-04-17 出版日期:2017-10-15 发布日期:2017-04-17
通讯作者: 董宏洋 E-mail:donghongyang91@gmail.com
基金资助:
国家自然科学基金（61522301，61633003）

Fault-tolerant translational control for spacecraft formation flying with collision avoidance requirement

MA Guangfu¹, DONG Hongyang¹, HU Qinglei²

1. School of Astronautics, Harbin Institute of Technology, Harbin 150001, China;
2. School of Automation Science and Electrical Engineering, Beihang University, Beijing 100083, China

Received:2017-01-13 Revised:2017-04-17 Online:2017-10-15 Published:2017-04-17
Supported by:
National Natural Science Foundation of China (61522301, 61633003)

摘要/Abstract

摘要：

为解决航天器编队飞行过程中的故障容错、障碍规避以及碰撞避免等重要的飞行安全问题，提出了一种新颖的自适应轨道控制方法。该方法将人工势函数制导与滑模控制技术相结合，利用一类特殊的人工势函数来描述障碍规避及碰撞避免等要求，并基于此为航天器编队设计了协同控制器，使得编队在实现目标追踪和构型保持的同时，能够避免相互碰撞并具备规避障碍物的能力。更为重要的是，控制器中自适应律的引入使得闭环系统对执行机构故障、外界干扰及参数不确定性具备良好的容错能力，显著增强了闭环系统的鲁棒性。最后，典型的仿真分析验证了所提控制方法的有效性。

关键词: 航天器编队控制, 容错控制, 人工势函数制导, 障碍规避, 碰撞避免

Abstract:

To solve the flying safety issues of spacecraft formation,including fault tolerance and obstacle/collision avoidance,a novel adaptive translational control method is proposed.Specifically,the proposed method combines the core ideas of artificial potential function guidance and sliding mode control method.A special artificial potential function is designed to encode the collision/obstacle avoidance requirement,and then a coordination controller is presented to enable the spacecraft formation to maintain the predetermined configuration while tracking a target,and to be able to avoid all possible collisions between members in formation or with respect to a non-cooperative obstacle.Furthermore,by introducing adaptive laws into the controller,the robustness of the closed-loop system is further improved in respect to external disturbances,parameter uncertainties and even severe actuator faults.Typical simulations are performed to illustrate the effectiveness of the proposed method.

Key words: spacecraft formation flying control, fault-tolerant control, artificial potential function guidance, obstacle avoidance, collision avoidance

中图分类号:

V412.4⁺1

马广富, 董宏洋, 胡庆雷. 考虑避障的航天器编队轨道容错控制律设计[J]. 航空学报, 2017, 38(10): 321129-321129.

MA Guangfu, DONG Hongyang, HU Qinglei. Fault-tolerant translational control for spacecraft formation flying with collision avoidance requirement[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(10): 321129-321129.

参考文献

[1] KAPILA V, SPARKS A G, BUFFINGTON J M, et al. Spacecraft formation flying:Dynamics and control[J]. Journal of Guidance, Control, and Dynamics, 2000, 23(3):561-564.
[2] REN W, BEARD R. Decentralized scheme for spacecraft formation flying via the virtual structure approach[J].Journal of Guidance,Control, and Dynamics, 2004, 27(1):73-82.
[3] BREAD R W, LAWTON J, HOW J P. A coordination architecture for spacecraft formation control[J]. IEEE Transactions on Control Systems Technology, 2001, 9(6):777-790.
[4] WANG P K C, HADAEGH F Y. Coordination and control of multiple microspacecraft moving in formation[J]. Journal of the Astronautical Scineces, 1996, 44(3):315-335.
[5] CANUTO E, COLANGELO L, LOTUFO M, et al. Satellite-to-satellite attitude control of a long-distance spacecraft formation for the next generation gravity mission[J]. European Journal of Control, 2015, 25(5):1-16.
[6] ZHOU N, XIA Y Q. Coordination control design for formation reconfiguration of multiple spacecraft[J]. IET Control Theory and Applications, 2015, 9(15):2222-2231.
[7] 郑重, 宋申民. 考虑避免碰撞的编队卫星自适应协同控制[J]. 航空学报, 2013, 34(8):1934-1943. ZHENG Z, SONG S M. Adaptive coordination control of satellites within formation considering collision avoidance[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(8):1934-1943(in Chinese).
[8] HU Q L, DONG H Y, ZHANG Y M, et al. Tracking control of spacecraft formation flying with collision avoidance[J]. Aerospace Science and Technology, 2015, 42:353-364.
[9] ZHANG D, SONG S, PEI R. Safe guidance for autonomous rendezvous and docking with a noncooperative target[C]//AIAA Guidance, Navigation, and Control Conference. Reston, VA:AIAA, 2010.
[10] VARMA S, KUMAR K D. Fault tolerant satellite attitude control using solar radiation pressure based on nonlinear adaptive sliding mode[J]. Acta Astronautica, 2009, 66(3-4):486-500.
[11] RUITER A D. A fault tolerant magnetic spin stabilizing controller for JC2Sat-FF mission[J]. Acta Astronautica, 2011, 68(1-2):160-171.
[12] JIN J, KO S, RYOO C K. Fault tolerant control for satellites with four reaction wheels[J]. Control Engineering Practice, 2008, 16(10):1250-1258.
[13] CAI W, LIAO X, SONG D Y. Indirect robust adaptive fault-tolerant control for attitude tracking of spacecraft[J]. Journal of Guidance, Control, and Dynamics, 2012, 31(5):1456-1463.
[14] XIAO B, HU Q, ZHANG Y. Finite-time attitude tracking of spacecraft with fault-tolerant capability[J]. IEEE Transactions on Control Systems Technology, 2015, 23(4):1338-1350.
[15] DONG H Y, HU Q L, MA G F. Dual-quaternion based fault-tolerant control for spacecraft formation flying with finite-time convergence[J]. ISA Transactions, 2016, 61(99):87-94.
[16] SINGLA P, SUBBARAO K, JUNKINS J L. Adaptive output feedback control for spacecraft rendezvous and docking under measurement uncertainty[J]. Journal of Guidance, Control, and Dynamics, 2006, 29(4):892-902.
[17] KRISTIANSEN R, NICKLASSON P J. Spacecraft formation flying:A review and new results on state feedback control[J]. Acta Astronautica, 2009, 65(11-12):1537-1552.
[18] MURUGESAN S, GOEL P S. Fault-tolerant spacecraft attitude control system[J]. Sadhana, 1987, 11(1-2):233-261.
[19] RIMON E, KODITSCHEK D E. Exact robot navigation using artificial potential functions[J]. IEEE Transactions on Robotics and Automation, 1992, 8(5):501-518.
[20] BADAWY A, MCINNES C R. Small spacecraft formation using potential function[J]. Acta Astronautica, 2009, 65(11-12):1783-1788.
[21] GAZI V, ORDONEZ R. Target tracking using artificial potentials and sliding mode control[J]. International Journal of Control, 2007, 80(10):1626-1635.
[22] ZHANG F. The schur complement and its applications[M]. New York:Springer, 2006:17-46.
[23] LIU X F, LU P. Solving nonconvex optimal control problems by convex optimization[J]. Journal of Guidance, Control, and Dynamics, 2014, 37(3):750-765.

E-mail：hkxb@buaa.edu.cn

关于我们

期刊社服务

专业学科

封面文章

友情链接

主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

考虑避障的航天器编队轨道容错控制律设计

Fault-tolerant translational control for spacecraft formation flying with collision avoidance requirement

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	杨晓伟, 葛曜文, 邓文翔, 姚建勇, 周宁. 航空发动机导叶控制机构作动筒主动容错控制[J]. 航空学报, 2022, 43(9): 625464-625464.
[2]	胡庆雷, 邵小东, 杨昊旸, 段超. 航天器多约束姿态规划与控制:进展与展望[J]. 航空学报, 2022, 43(10): 527351-527351.
[3]	黄旭星, 李爽, 杨彬, 孙盼, 刘学文, 刘新彦. 人工智能在航天器制导与控制中的应用综述[J]. 航空学报, 2021, 42(4): 524201-524201.
[4]	刘德元, 刘昊, Frank L LEWIS. 尾座式无人飞行器鲁棒容错编队控制[J]. 航空学报, 2021, 42(2): 324296-324296.
[5]	姜斌, 张柯, 杨浩, 程月华, 马亚杰, 成旺磊. 卫星姿态控制系统容错控制综述[J]. 航空学报, 2021, 42(11): 524662-524662.
[6]	梅亚飞, 廖瑛, 龚轲杰, 罗达. SE(3)上航天器姿轨耦合固定时间容错控制[J]. 航空学报, 2021, 42(11): 525089-525089.
[7]	司宾强, 黄玉平, 朱纪洪, 于航. 高可靠电机系统主动变结构与容错控制技术[J]. 航空学报, 2021, 42(11): 524853-524853.
[8]	葛佳昊, 刘莉, 董欣心, 田维勇, 陆天和. 基于动力学RRT^*的自由漂浮空间机器人轨迹规划[J]. 航空学报, 2021, 42(1): 523877-523877.
[9]	邵书义, 陈谋, 招启军. 基于干扰观测器的四旋翼无人机离散时间容错控制[J]. 航空学报, 2020, 41(S2): 724283-724283.
[10]	董旺, 齐瑞云, 姜斌. 空天飞行器直接力/气动力复合容错控制[J]. 航空学报, 2020, 41(11): 623850-623850.
[11]	余诗怡, 郝振洋. 航空发动机内置式永磁容错发电系统的研究[J]. 航空学报, 2016, 37(9): 2775-2787.
[12]	董朝阳, 路遥, 江未来, 王青. 基于布谷鸟搜索算法的一类变体飞行器容错控制[J]. 航空学报, 2015, 36(6): 2047-2054.
[13]	胡庆雷, 姜博严, 石忠. 基于新型终端滑模的航天器执行器故障容错姿态控制[J]. 航空学报, 2014, 35(1): 249-258.
[14]	胡庆雷, 张爱华, 李波. 推力器故障的刚体航天器自适应变结构容错控制[J]. 航空学报, 2013, 34(4): 909-918.
[15]	肖冰, 胡庆雷, 霍星, 马广富. 执行器故障的挠性航天器姿态滑模容错控制[J]. 航空学报, 2011, 32(10): 1869-1878.