Three-dimensional adaptive finite-time super-twisting sliding mode guidance law

被引:0
|
作者
Li J. [1 ]
Liao Y. [1 ]
Li J. [1 ]
机构
[1] School of Aeronautics and Astronautics, Central South University, Changsha
关键词
Finite-time convergence; Nonsingular fast terminal sliding mode; Super-twisting algorithm; Terminal attack angle constraint; Three-dimensional interception guidance law;
D O I
10.12305/j.issn.1001-506X.2021.03.23
中图分类号
学科分类号
摘要
Aiming at the guidance problem of intercepting maneuvering target with fixed terminal attack angle, a three-dimensional adaptive finite-time super-twisting sliding mode guidance law is proposed. Firstly, the three-dimensional guidance problem is transformed into the control problem of the second-order line-of-sight angle system by using the relative motion particle model. Secondly, a multi-variable nonsingular fast terminal sliding surface is constructed, and the finite-time super-twisting sliding mode guidance law is designed by combining the improved super-twisting algorithm. At the same time, the upper bound of external disturbance caused by target maneavering is estimated online by parameter adaptive gain, and the adaptive finite-time super-twisting sliding mode guidance law is designed. Then, the finite-time convergence performance of the closed-loop system is analyzed by using the Lyapunov stability theory. Finally, the simulation results show that the proposed method has better robustness and higher terminal attack angle control accuracy while ensuring good interception accuracy. © 2021, Editorial Office of Systems Engineering and Electronics. All right reserved.
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页码:779 / 788
页数:9
相关论文
共 26 条
  • [1] LIU B J, HOU M S, YU Y., Guidance law with impact angle constraints based on immersion and invariance, Systems Engineering and Electronics, 40, 5, pp. 1085-1090, (2018)
  • [2] CHEN X T, WANG J Z., Optimal control based guidance law to control both impact time and impact angle, Aerospace Science and Technology, 84, pp. 454-463, (2019)
  • [3] LI C D, WANG J, LI B, Et al., Energy-optimal guidance law with virtual hand-over point, Acta Aeronautica Et Astronautica Sinica, 40, 12, pp. 178-187, (2019)
  • [4] MENG K Z, ZHOU D., Design of optimal midcourse guidance law with multiple constraints, Systems Engineering and Electronics, 38, 1, pp. 116-122, (2016)
  • [5] SUN J L, LIU C S, YE Q., Robust differential game guidance laws design for uncertain interceptor-target engagement via adaptive dynamic programming, International Journal of Control, 90, 5, pp. 990-1004, (2017)
  • [6] LI W, HUANG R S, WANG F, Et al., Nonlinear differential games guidance law based on SDRE with terminal impact angular, Systems Engineering and Electronics, 38, 7, pp. 1606-1613, (2016)
  • [7] SUN L H, WANG W H, YI R, Et al., A novel guidance law using fast terminal sliding mode control with impact angle constraints, ISA Transactions, 64, pp. 12-23, (2016)
  • [8] SONG J H, SONG S M, GUO Y, Et al., Nonlinear disturbance observer-based fast terminal sliding mode guidance law with impact angle constraints, International Journal of Innovative Computing Information and Control, 11, 3, pp. 787-802, (2015)
  • [9] WANG C L, SONG B H, CHANG C., Nonsingular finite-time guidance law with missile dynamic, Journal of National University of Defense Technology, 40, 2, pp. 22-27, (2018)
  • [10] ZHAO G R, LI X B, LIU S, Et al., Adaptive nonsingular fast terminal sliding mode guidance law with fixed-time convergence, Journal of Beijing University of Aeronautics and Astronautics, 45, 6, pp. 1059-1070, (2019)