Guidance law implementation with performance recovery using an extended high-gain observer

被引：31
作者：
Ma, Kemao [1 ]
Khalil, Hassan K. [2 ]
Yao, Yu [1 ]
机构：
[1] Harbin Inst Technol, Sch Astronaut, Control & Simulat Ctr, Harbin 150080, Peoples R China
[2] Michigan State Univ, Dept Elect & Comp Engn, E Lansing, MI 48823 USA
来源：
AEROSPACE SCIENCE AND TECHNOLOGY | 2013年 / 24卷 / 01期
基金：
中国国家自然科学基金; 美国国家科学基金会;
关键词：
Guidance law; Target maneuver; High-gain observer; Performance recovery; PARTIAL STABILITY; HOMING MISSILE; STABILIZATION;
D O I：
10.1016/j.ast.2011.11.005
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Guidance law of a homing missile is implemented using an extended high gain observer without the model assumptions on target maneuvers. First, for a class of multi-input-multi-output nonlinear systems, extended high-gain observers are used for output feedback control with partial practical stabilization. Then the method is applied to the guidance law implementation of a homing missile with bearing only measurement. Simulation results show satisfactory performance. (C) 2011 Elsevier Masson SAS. All rights reserved.
引用
收藏
页码：177 / 186
页数：10
相关论文
共 50 条
  • [31] Dynamic inversion-based hysteresis compensation using extended high-gain observe
    Chowdhury, Dhrubajit
    Al-Nadawi, Yasir K.
    Tan, Xiaobo
    AUTOMATICA, 2022, 135
  • [32] Output feedback Controller using High-Gain Observer in Multi-Motor Drive Systems
    Dao Phuong Nam
    Pham Tuan Thanh
    Tran Xuan Tinh
    2017 INTERNATIONAL CONFERENCE ON SYSTEM SCIENCE AND ENGINEERING (ICSSE), 2017, : 428 - 431
  • [33] Robust output feedback controller with high-gain observer for automatic clutch
    Shi, Jialei
    Li, Liang
    Wang, Xiangyu
    Liu, Congzhi
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2019, 132 : 806 - 822
  • [34] Time-Varying High-Gain Trajectory Linearization Observer Design
    Huang, Rui
    Zhu, J. Jim
    2009 AMERICAN CONTROL CONFERENCE, VOLS 1-9, 2009, : 4628 - 4635
  • [35] High-gain interval observer for partially linear systems with bounded disturbances
    Thabet, Rihab El Houda
    Ali, Sofiane Ahmed
    Puig, Vicenc
    INTERNATIONAL JOURNAL OF CONTROL, 2021, 94 (05) : 1376 - 1385
  • [36] Sliding Mode Control for VTOL Aircraft Based on High-Gain Observer
    Gong Haisheng
    Liu Jinkun
    PROCEEDINGS OF THE 2012 SECOND INTERNATIONAL CONFERENCE ON INSTRUMENTATION & MEASUREMENT, COMPUTER, COMMUNICATION AND CONTROL (IMCCC 2012), 2012, : 305 - 309
  • [37] Design and implementation of a sliding-mode controller and a high-gain observer for output tracking of a three-axis pickup
    Chao, Paul C. -P.
    Shen, Chien-Yu
    SENSORS AND ACTUATORS A-PHYSICAL, 2007, 135 (02) : 713 - 730
  • [38] An Improved Equivalent-Input-Disturbance Approach for Disturbance-Rejection Using High-Gain Observer
    Du, Youwu
    Cao, Weihua
    She, Jinhua
    Fang, Mingxing
    Lu, Zibao
    2018 37TH CHINESE CONTROL CONFERENCE (CCC), 2018, : 2643 - 2647
  • [39] On the performance of high-gain observers with gain adaptation under measurement noise
    Sanfelice, Ricardo G.
    Praly, Laurent
    AUTOMATICA, 2011, 47 (10) : 2165 - 2176
  • [40] Motion Control of Towed Underwater Vehicles with Movable Wings Using a High-Gain Observer Based Approach
    Minowa, Asuma
    Toda, Masayoshi
    PROCEEDINGS OF THE 2015 10TH IEEE CONFERENCE ON INDUSTRIAL ELECTRONICS AND APPLICATIONS, 2015, : 1887 - 1892
12345