Distance-Scalar Disturbance Observer-Based Parallel Approaching Guidance Using Finite-Time Prescribed Performance

被引:0
作者
Sun, Haoxuan [1 ]
Yong, Kenan [1 ]
Shen, Yaohua [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Automat Engn, Nanjing 210016, Peoples R China
关键词
finite-time prescribed performance control; nonlinear disturbance observer; parallel approaching guidance; LAW;
D O I
10.3390/aerospace10110936
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this paper, to make an interceptor intercept a maneuvering target, a parallel approaching guidance law is developed. In order to estimate the target maneuver more accurately and reduce its influence on the guidance accuracy, a distance-scalar disturbance observer is employed. Specifically, the estimation accuracy of the designed observer is not affected by the relative distance. Finite-time prescribed performance is employed to ensure that the line-of-sight angular rate is capable of converging to a predetermined small region within the specified finite time. All signals of the interception system can guarantee an ultimately uniformly boundedness, as proven by Lyapunov stability theory. Finally, the function of the parallel approaching guidance law is demonstrated using numerical simulation.
引用
收藏
页数:19
相关论文
共 36 条
  • [1] Nonlinear Differential Games-Based Impact-Angle-Constrained Guidance Law
    Bardhan, Rajarshi
    Ghose, Debasish
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2015, 38 (03) : 384 - 402
  • [2] Bechlioulis CP, 2008, MED C CONTR AUTOMAT, P21
  • [3] A Simplified Finite-Time Fuzzy Neural Controller With Prescribed Performance Applied to Waverider Aircraft
    Bu, Xiangwei
    Qi, Qiang
    Jiang, Baoxu
    [J]. IEEE TRANSACTIONS ON FUZZY SYSTEMS, 2022, 30 (07) : 2529 - 2537
  • [4] Nonlinear fuzzy H∞ guidance law with saturation of actuators against maneuvering targets
    Chen, BS
    Chen, YY
    Lin, CL
    [J]. IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2002, 10 (06) : 769 - 779
  • [5] Adaptive Neural Fault-Tolerant Control of a 3-DOF Model Helicopter System
    Chen, Mou
    Shi, Peng
    Lim, Cheng-Chew
    [J]. IEEE TRANSACTIONS ON SYSTEMS MAN CYBERNETICS-SYSTEMS, 2016, 46 (02): : 260 - 270
  • [6] CONSTRAINED INITIAL GUIDANCE ALGORITHM
    COCHRAN, JE
    HAYNES, DA
    [J]. JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1990, 13 (02) : 193 - 197
  • [7] Proportional Navigation With Delayed Line-of-Sight Rate
    Dhananjay, N.
    Lum, Kai-Yew
    Xu, Jian-Xin
    [J]. IEEE TRANSACTIONS ON CONTROL SYSTEMS TECHNOLOGY, 2013, 21 (01) : 247 - 253
  • [8] Output Feedback Approximation-Free Prescribed Performance Tracking Control for Uncertain MIMO Nonlinear Systems
    Dimanidis, Ioannis S.
    Bechlioulis, Charalampos P.
    Rovithakis, George A.
    [J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 2020, 65 (12) : 5058 - 5069
  • [9] Fei D., 2022, Aerosp. Sci. Technol, V131, P107974
  • [10] A trajectory shaping guidance law with field-of-view angle constraint and terminal limits
    Fu Shengnan
    Zhou Guanqun
    Xia Qunli
    [J]. JOURNAL OF SYSTEMS ENGINEERING AND ELECTRONICS, 2022, 33 (02) : 426 - 437