The Anti-Windup Control for Hypersonic Vehicles with Input Saturation Based on Improved Cooperative Optimization Algorithm

被引:0
|
作者
Sun, Ping [1 ]
Du, Yanli [1 ]
Zhang, Peng [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Astronaut, Nanjing, Jiangsu, Peoples R China
关键词
hypersonic vehicle; anti-windup compensation; L2; gain; nonlinear matrix inequality; improved cooperative optimization algorithm;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
A nonlinear anti-windup(AW) control compensator based on improved cooperative optimization algorithm(ICOA) is proposed to deal with the control problem caused by the saturation of the control surfaces of the hypersonic vehicle(HSV) during re-entry. Firstly, saturated link is added in the system controller, and the model of AW compensator is designed according to the HSV system equations. Then, the nonlinear L2 gain structure is introduced with the purpose of optimizing the performance of system, which transforms the problem of saturation control into the optimization problem through nonlinear matrix inequality (NMIL) constraints. The optimization problem is solved by an ICOA. Finally, the simulation results show the effectiveness of the proposed method. The saturation situation can be relieved within a short time and the satisfactory control performance is attained by the presented method.
引用
收藏
页码:313 / 318
页数:6
相关论文
共 50 条
  • [1] The Nonlinear Anti-Windup Control of Hypersonic Glide Vehicles with Input Saturation and Uncertainties
    Sun Ping
    Du Yanli
    Zhang Peng
    Xiang Kai
    [J]. 2017 29TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2017, : 4631 - 4637
  • [2] Anti-windup Control for Near Space Vehicles subject to Input Saturation
    Yang, Qingyun
    Chen, Mou
    [J]. 2014 33RD CHINESE CONTROL CONFERENCE (CCC), 2014, : 3760 - 3765
  • [3] Fault-tolerant anti-windup control for hypersonic vehicles in reentry based on ISMDO
    Meng, Yizhen
    Jiang, Bin
    Qi, Ruiyun
    Liu, Jianwei
    [J]. JOURNAL OF THE FRANKLIN INSTITUTE-ENGINEERING AND APPLIED MATHEMATICS, 2018, 355 (05): : 2067 - 2090
  • [4] Anti-Windup Switched Control of Hypersonic Vehicle
    Liu T.-H.
    An H.
    Wang C.-H.
    [J]. Wang, Chang-Hong (cwang@hit.edu.cn), 1600, China Spaceflight Society (41): : 329 - 336
  • [5] Intelligent anti-windup for systems with input magnitude saturation
    Burgat, C
    Tarbouriech, S
    [J]. INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL, 1998, 8 (12) : 1085 - 1100
  • [6] An anti-windup design for linear systems with input saturation
    Kapoor, N
    Teel, AR
    Daoutidis, P
    [J]. AUTOMATICA, 1998, 34 (05) : 559 - 574
  • [7] An Internal Model Control Anti-Windup Scheme With Improved Performance for Input Saturation Via Loop Shaping
    Wu, Wei
    Jayasuriya, Suhada
    [J]. JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 2010, 132 (01): : 1 - 6
  • [8] An internal model control based anti-windup scheme for stable uncertain plants with input saturation
    Wu, Wei
    Jayasuriya, Suhada
    [J]. PROCEEDINGS OF THE 45TH IEEE CONFERENCE ON DECISION AND CONTROL, VOLS 1-14, 2006, : 5424 - 5428
  • [9] RBFNN-Based Anti-Input Saturation Control for Hypersonic Vehicles
    Zhang, Bangchu
    Liang, Yiyong
    Rao, Shuitao
    Kuang, Yu
    Zhu, Weiyu
    [J]. AEROSPACE, 2024, 11 (02)
  • [10] Design of model-based Anti-Windup Methods for Systems with Input Saturation
    Ortseifen, Andreas
    [J]. AT-AUTOMATISIERUNGSTECHNIK, 2014, 62 (03) : 237 - 238