Guardian maps based robust stability analysis with applications in flight control of hypersonic vehicles

被引:5
|
作者
Chen, Boyi [1 ]
Chen, Jinbao [1 ]
Liu, Yanbin [1 ]
Lei, Hao [1 ]
Jia, Shan [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Nanjing, Peoples R China
基金
中国国家自然科学基金;
关键词
Guardian maps; Multi-parametric uncertainty; Parametric stability margin; Robust stability; Hypersonic vehicles; SYSTEMS;
D O I
10.1016/j.ast.2020.106208
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Guardian maps provide a concise and practical approach to parametric robustness analysis. However, non-convexity and nonlinearity of high dimensional guardian maps restrict the application. In this paper, a closed-loop performance-oriented approach to parametric robustness analysis is proposed. First, a sufficient condition for the existence of parametric stable region satisfying the closed-loop performance is presented. To further identify the maximum stable region, a robustness criterion is provided, leading to a numerical approach for parametric stability margin. The superiority of the proposed method lies in the applicability to robust performance analysis with nonlinear high-dimensional parameters. Applications are discussed with emphasis on the flight control of hypersonic vehicles, including robust control design and robust stability analysis. Results are of significant that no prior knowledge on controller tuning is required, and parametric stability margin can be obtained automatically regardless of the dimension of parameter space. (C) 2020 Elsevier Masson SAS. All rights reserved.
引用
收藏
页数:11
相关论文
共 50 条
  • [1] A Design Method of Switching Control for Hypersonic Vehicles Based on Guardian Maps
    Xiao Dibo
    Chen Boyi
    Liu Yanbin
    Liu Mengying
    Lu Yuping
    2015 34TH CHINESE CONTROL CONFERENCE (CCC), 2015, : 5658 - 5662
  • [2] Guardian Maps Based Switching Tracking Control of Large Envelope Hypersonic Vehicles
    Shen Haidong
    Liu Kai
    Chen Boyi
    Liu Yanbin
    Lu Yuping
    PROCEEDINGS OF THE 35TH CHINESE CONTROL CONFERENCE 2016, 2016, : 10657 - 10661
  • [3] Adaptive Control of Hypersonic Vehicles using Guardian Maps Theory
    Liu Mengying
    She Zhiyong
    Xiao Dibo
    Liu Yanbin
    Luo Delin
    2015 34TH CHINESE CONTROL CONFERENCE (CCC), 2015, : 5653 - 5657
  • [4] Robust Stabilization Control Based on Guardian Maps Theory for a Longitudinal Model of Hypersonic Vehicle
    Liu, Yanbin
    Liu, Mengying
    Sun, Peihua
    SCIENTIFIC WORLD JOURNAL, 2014,
  • [5] Switching control of a hypersonic vehicle based on guardian maps
    Xiao, Dibo
    Liu, Mengying
    Liu, Yanbin
    Lu, Yuping
    ACTA ASTRONAUTICA, 2016, 122 : 294 - 306
  • [6] Adaptive control law design using guardian maps theory for hypersonic vehicles
    Xiao, Dibo
    Lu, Yuping
    Liu, Yanbin
    Xu, Chen
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2015, 36 (10): : 3327 - 3337
  • [7] Coordinated attitude control of hypersonic flight vehicles based on the coupling analysis
    Zhen, Wubin
    Wang, Yuhui
    Wu, Qingxian
    Shao, Peng
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2018, 232 (05) : 1002 - 1011
  • [8] Feedback linearization-based robust nonlinear control design for hypersonic flight vehicles
    Rehman, Obaid Ur
    Petersen, Ian R.
    Fidan, Baris
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART I-JOURNAL OF SYSTEMS AND CONTROL ENGINEERING, 2013, 227 (I1) : 3 - 11
  • [9] Nonlinear-Disturbance-Observer-Based Robust Flight Control for Airbreathing Hypersonic Vehicles
    Yang, Jun
    Li, Shihua
    Sun, Changyin
    Guo, Lei
    IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 2013, 49 (02) : 1263 - 1275
  • [10] Robust LMI Control for Hypersonic Flight Vehicles Based on Specified Region Pole Assignment
    Li Huifeng
    Zhao Liting
    PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2, 2010, : 620 - 623