故障自适应滑模再入姿态控制设计

doi:10.3969/j.issn.1009-086x.2018.06.008

现代防御技术 ›› 2018, Vol. 46 ›› Issue (6): 51-56.DOI: 10.3969/j.issn.1009-086x.2018.06.008

故障自适应滑模再入姿态控制设计

韩嘉俊^{1, 2}, 王小虎³, 吴旭忠¹

1. 北京机电工程总体设计部, 北京 100854;
2. 中国航天科工集团有限公司第二研究院, 北京 100854;
3. 北京控制与电子技术研究所, 北京 100038

出版日期:2018-11-30 发布日期:2020-10-22
作者简介:韩嘉俊(1990-), 男, 山西阳泉人。博士生, 主要研究方向为导航制导与控制。通信地址:100854 北京市142信箱206分箱 E-mail:nuaa101h@126.com

Reentry Attitude Control Based on Fault Adaptive Sliding Mode Control

HAN Jia-jun^{1, 2}, WANG Xiao-hu³, WU Xu-zhong¹

1.Beijing System Design Institute of Electro-Mechanic Engineering, Beijing 100854, China;
2.The Second Research Academy of CASIC, Beijing 100854, China;
3.Beijing Institute of Control and Electronic Technology, Beijing 100038, China

Online:2018-11-30 Published:2020-10-22

摘要/Abstract

摘要： 为了解决再入飞行过程中, 飞行器故障时的姿态控制问题。提出了一种故障检测策略和在故障状态下的姿态控制方法。首先, 设计了非线性故障检测观测器, 通过姿态角观测误差阈值确定故障是否发生。其次, 使用自适应控制技术和滑模控制技术实现了故障情况下的再入飞行器姿态控制。最后, 通过数值仿真算例, 测试了经典双回路控制律和提出的容错控制律下的姿态指令跟踪效果, 证明了提出的容错控制策略的有效性。

关键词: 再入滑翔, 姿态控制, 滑模观测器, 故障检测, 容错控制

Abstract: In order to satisfy the requirements of reentry vehicle attitude control under the uncertain fault and improve the robustness and adaptability of reentry control, a fault detection strategy and a attitude control method with actuator fault are introduced.For the dynamic model of reentry vehicle in fault case, a fault detection scheme is proposed by designing a nonlinear fault detection observer.An active tolerant tracking strategy is presented by making use of both adaptive control and sliding mode control techniques.Finally, simulation results are given to demonstrate the effectives of the developed fault tolerant control scheme.

Key words: reentry glide, attitude control, slide mode observer, fault diagnosis, fault tolerant control

中图分类号:

韩嘉俊, 王小虎, 吴旭忠. 故障自适应滑模再入姿态控制设计[J]. 现代防御技术, 2018, 46(6): 51-56.

HAN Jia-jun, WANG Xiao-hu, WU Xu-zhong. Reentry Attitude Control Based on Fault Adaptive Sliding Mode Control[J]. Modern Defense Technology, 2018, 46(6): 51-56.

参考文献 15

[1]	SHTESSEL Y, STOTT J, ZHU J.Time-Varying Sliding Mode Control with Sliding Mode Observer for Reusable Launch Vehicle[C]∥AIAA Guidance, Navigation, and Control Conference and Exhibit, 2003, 235-243.
[2]	SHTESSEL Y, ZHU J, DANIELS D.Reusable Launch Vehicle Attitude Control Using Time-Varying Sliding Modes[C]∥AIAA Guidance, Navigation, and Control Conference and Exhibit, 2002:81-85.
[3]	QUANG L, PRASHANTH K, FARSHAD K.Enhancing Flight Control System Performance Using SDRE Based Controller as an Augmentation Layer[C]∥AIAA Guidance, Navigation, and Control Conference, 2009:346-359.
[4]	XIN M, BALAKRISHNAN S.State Dependent Riccati Equation Based Spacecraft Attitude Control[C]∥40th AIAA Aerospace Sciences Meeting & Exhibit, 2002:91-98.
[5]	DE RUITER A H J.Adaptive Spacecraft Attitude Control with Actuator Saturation[J].Journal of Guidance, Control, and Dynamics, 2010, 33(5):1692-1696.
[6]	CHAE-JK A, YOUDAN K, HYOUNJIN K.Adaptive Sliding Mode Controller Design for Fault Tolerant Flight Control System[C]∥AIAA Guidance, Navigation, and Control Conference and Exhibit, 2006:614-650.
[7]	BINGLONG C, XIANGDONG L, ZHEN C.Exponential Time-Varying Sliding Mode Control for Large Angle Attitude Eigenaxis Maneuver of Rigid Spacecraft[J].Chinese Journal of Aeronautics, 2010, 23(4):447-453.
[8]	SHEN Y, HUANG Y.Global finite-time stabilisation for a Class of Nonlinear Systems[J].International Journal of Systems Science, 2012, 43(1):73-78.
[9]	GAO Z, JIANG B, SHI P, et al.Active Fault Tolerant Control Design for Reusable Launch Vehicle Using Adaptive Sliding Mode Technique[J].Journal of the Franklin Institute, 2012, 349(4):1543-1560.
[10]	STENGEL R F, HANDELMAN D A.Combining Expert System and Analytical Redundancy Concepts for Fault-Tolerant Flight Control[J].Journal of Guidance Control & Dynamics, 2012, 12(1):39-45.
[11]	FALCOZ A, HENRY D, ZOLGHADRI A.Robust Fault Diagnosis for Atmospheric Reentry Vehicles:A Case Study[J].Systems, Man and Cybernetics, Part A:Systems and Humans, IEEE Transactions on, 2010, 40(5):886-899.
[12]	GAO Z, JIANG B, SHI P, et al.Active Fault Tolerant Control Design for Reusable Launch Vehicle Using Adaptive Sliding Mode Technique[J].Journal of the Franklin Institute, 2012, 349(4):1543-1560.
[13]	SUN H, LI S, SUN C.Finite Time Integral Sliding Mode Control of Hypersonic Vehicles[J].Nonlinear Dynamics, 2013, 73(1-2):229-244.
[14]	SHEN Z, LU P.Onboard Generation of Three-Dimensional Constrained Entry Trajectories[J].Journal of Guidance, Control, and Dynamics, 2003.26(1):111-121.
[15]	AGUSTIN R M, MANGOUBI R S, HAIN R M, et al.Robust Failure Detection for Reentry Vehicle Attitude Control Systems[J].Journal of Guidance, Control, and Dynamics, 1999, 22(6):839-845.

故障自适应滑模再入姿态控制设计

Reentry Attitude Control Based on Fault Adaptive Sliding Mode Control

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