Research on Three-Dimensional Integrated Guidance and Control Design with Multiple Constraints

被引:2
|
作者
Fu, Zhenhua [1 ]
Zhang, Kuanqiao [2 ]
Yang, Suochang [3 ]
机构
[1] Beijing Inst Technol, Sch Automat, Beijing, Peoples R China
[2] State Key Lab Complex Electromagnet Environm Effe, Luoyang, Peoples R China
[3] Army Engn Univ, Shijiazhuang, Hebei, Peoples R China
关键词
SLIDING MODE CONTROL; IMPACT ANGLE; MISSILE;
D O I
10.1155/2022/6296770
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper, a fixed-time convergence-integrated guidance and control (IGC) method is proposed, which considers terminal line-of-sight (LOS) angle constraint, full-state constraints, and input saturation. Firstly, an IGC design model considering the full coupling of three channels is constructed, and a fixed-time convergence disturbance observer is used to estimate and compensate the unknown disturbances in the model. Secondly, based on the fixed-time stability theory, sliding mode control, and backstepping control, a novel IGC scheme is carried out, and the second-order instruction filter is used to restrict the system states and control instructions. Furthermore, the fixed-time stability of the close-loop system is proved and the expression of convergence time upper bound is given. Finally, comparison simulation and Monte Carlo simulation verify the effectiveness and superiority of the proposed IGC algorithm.
引用
收藏
页数:18
相关论文
共 50 条
  • [21] Design of a three-dimensional CLOS guidance law via sliding mode control
    Cai, Peng
    Wang, Qing-Chao
    Yuhang Xuebao/Journal of Astronautics, 2007, 28 (06): : 1651 - 1655
  • [22] Three-Dimensional Integrated Guidance and Control for BTT Aircraft Constrained by Terminal Flight Angles
    Liu, Xiaodong
    Huang, Wanwei
    Du, Lifu
    Lan, Pengjie
    Sun, Yong
    2015 27TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2015, : 107 - 112
  • [23] Three-Dimensional Integrated Guidance and Control for a STT Missile Based on Improved RISE in Series
    Ju, Tan
    Yu, Jiyan
    Ming, Chao
    Wang, Xiaoming
    Gu, Xiaohui
    IEEE ACCESS, 2019, 7 : 137887 - 137899
  • [24] Design of Three-dimensional Incremental Disturbance Compensation Guidance Law Considering Terminal Angle Constraints
    Hu, Jintao
    Hu, Qinglei
    Han, Tuo
    Yuhang Xuebao/Journal of Astronautics, 2024, 45 (09): : 1456 - 1466
  • [25] Three-Dimensional Guidance for Various Target Motions With Terminal Angle Constraints Using Twisting Control
    Hu, Qinglei
    Han, Tuo
    Xin, Ming
    IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2020, 67 (02) : 1242 - 1253
  • [26] Adaptive Backstepping Control for Integrated Guidance and Control Design with Input Constraints
    Liang, Xiaoling
    Liu, Yancheng
    Ding, Tiancheng
    Lu, Hengyu
    2016 31ST YOUTH ACADEMIC ANNUAL CONFERENCE OF CHINESE ASSOCIATION OF AUTOMATION (YAC), 2016, : 37 - 42
  • [27] Design of integrated guidance and control in space with multiple constraints of rolling naval gun guided projectile
    Jiang S.
    Tian F.
    Sun S.
    Liang W.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2019, 40 (10):
  • [29] A generalized design method for three-dimensional guidance laws
    Sun, Sheng
    Zhou, Di
    Zhou, Jingyang
    Teo, Kok Lay
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2017, 231 (01) : 47 - 60
  • [30] A Three-Dimensional Integrated Guidance Law for Rotary UAV Interception
    Zhu, Bing
    Xu, Juanjuan
    Bin Zaini, Abdul Hanif
    Xie, Lihua
    2016 12TH IEEE INTERNATIONAL CONFERENCE ON CONTROL AND AUTOMATION (ICCA), 2016, : 726 - 731