A probabilistic robust mixed H2/H∞ fuzzy control method for hypersonic vehicles based on reliability theory

被引：3
|
作者：
Yin, Xiaomeng [1 ]
Li, Xinming [2 ]
Liu, Lei [1 ]
Wang, Yongji [1 ]
Wei, Xing [1 ]
机构：
[1] Huazhong Univ Sci & Technol, Sch Automat, Natl Key Lab Sci & Technol Multispectral Informat, Wuhan 430074, Hubei, Peoples R China
[2] Beijing Aerosp Automat Control Inst, Beijing, Peoples R China
来源：
INTERNATIONAL JOURNAL OF ADVANCED ROBOTIC SYSTEMS | 2018年 / 15卷 / 01期
关键词：
Hypersonic vehicle; fuzzy control; reliability method; mixed H-2/H-infinity control; robust control; SLIDING-MODE CONTROL; SYSTEMS; DESIGN; AIRCRAFT; LQR;
D O I：
10.1177/1729881417754153
中图分类号：
TP24 [机器人技术];
学科分类号：
080202 ; 1405 ;
摘要：
Achieving balance between robustness and performance is always a challenge in the hypersonic vehicle flight control design. In this research, we focus on dealing with uncertainties of the fuzzy control system from the viewpoint of reliability. A probabilistic robust mixed H-2/H-infinity fuzzy control method for hypersonic vehicles is presented by describing the uncertain parameters as random variables. First, a Takagi-Sugeno fuzzy model is employed for the hypersonic vehicle nonlinear dynamics characteristics. Next, a robust fuzzy controller is developed by solving a reliability-based multi-objective linear matrix inequality optimization problem, in which the H-2/H-infinity performance is optimized under the condition that the system is robustly reliable to uncertainties. By this method, the system performance and reliability can be taken into account simultaneously, which reduces the conservatism in the robust fuzzy control design. Finally, simulation results of a hypersonic vehicle demonstrate the feasibility and effectiveness of the presented method.
引用
收藏
页数：15
相关论文
共 50 条
  • [1] Disturbance observer based robust mixed H2/H∞, fuzzy tracking control for hypersonic vehicles
    Wu, Huai-Ning
    Feng, Shuang
    Liu, Zhi-Yong
    Guo, Lei
    FUZZY SETS AND SYSTEMS, 2017, 306 : 118 - 136
  • [2] Mixed H2/H∞ robust adaptive control of hypersonic vehicles based on the characteristic model
    Huang, Huang
    Wang, Yong
    PROCEEDINGS OF THE 31ST CHINESE CONTROL CONFERENCE, 2012, : 2883 - 2888
  • [3] Numerical Solution Method for Mixed H2/H∞ Robust Control Problem Based on Wavelets
    张成科
    华东理工大学学报(自然科学版), 2004, (03) : 332 - 335
  • [4] Robust mixed H2/H∞ fuzzy control via static output feedback
    Min-Long Lin
    Ji-Chang Lo
    2006 IEEE INTERNATIONAL CONFERENCE ON SYSTEMS, MAN, AND CYBERNETICS, VOLS 1-6, PROCEEDINGS, 2006, : 1085 - +
  • [5] Robust Trajectory Tracking Design of Unmanned Aerial Vehicles via Nonlinear Mixed H2/H∞ Control Method
    Huang, Sean A.
    Chiang, Liang-An
    2015 10TH ASIAN CONTROL CONFERENCE (ASCC), 2015,
  • [6] Characteristic model-based H2/H∞ robust adaptive control during the re-entry of hypersonic cruise vehicles
    HUANG Huang
    ZHANG Zhao
    Science China(Information Sciences), 2015, 58 (01) : 201 - 221
  • [7] Characteristic model-based H2/H∞ robust adaptive control during the re-entry of hypersonic cruise vehicles
    Huang Huang
    Zhao Zhang
    Science China Information Sciences, 2015, 58 : 1 - 21
  • [8] Characteristic model-based H2/H∞ robust adaptive control during the re-entry of hypersonic cruise vehicles
    Huang Huang
    Zhang Zhao
    SCIENCE CHINA-INFORMATION SCIENCES, 2015, 58 (01) : 1 - 21
  • [9] Mixed H2 and H∞ optimal robust control design
    Sparks, Andrew G.
    Yeh, Hsi-Han
    Banda, Siva S.
    Optimal Control Applications and Methods, 1990, 11 (04) : 307 - 325
  • [10] Hybrid differential evolution method for the mixed H2/H∞ robust control problem
    Neumann, Donald
    de Araujo, Humberto X.
    2005 44TH IEEE CONFERENCE ON DECISION AND CONTROL & EUROPEAN CONTROL CONFERENCE, VOLS 1-8, 2005, : 1319 - 1324
12345