Integrated guidance and control of missile based on Nussbaum gain adaptive sliding mode control method

被引：0
|
作者：
Qi H. [1 ]
Zhang Z. [1 ]
Xu J.-T. [1 ]
Han P.-X. [2 ]
Zhang D.-W. [1 ]
机构：
[1] College of Aerospace and Civic Engineering, Harbin Engineering University, Harbin
[2] China Academy of Launch Vehicle Technology R&D Center, Beijing
来源：
Kongzhi yu Juece/Control and Decision | 2017年 / 32卷 / 01期
关键词：
Adaptive sliding-mode control; Integrated guidance and control; Nussbaum gain control; Uncertain model;
D O I：
10.13195/j.kzyjc.2015.1601
中图分类号：
学科分类号：
摘要：
Aiming at the problem of missile integrated guidance and control design, the Nussbaum gain adaptive sliding mode control method is proposed. Fully considering that the model of integrated guidance and control has the features of the channel coupling, the uncertainty of aerodynamic modeling, and the interference caused by the target maneuver and pneumatic parameters perturbation, based on the strong ability of adaptive control to identify unknown quantities, the ability of the sliding-mode control law to resist interference, and the control ability of the Nussbaum gain adaptive control to the system with uncertain coefficients, the Nussbaum gain adaptive sliding-mode control law is designed, and the stability of the system is proved. The simulation results show the effectiveness of the proposed method. © 2017, Editorial Office of Control and Decision. All right reserved.
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页码：93 / 99
页数：6
相关论文
共 19 条
  • [1] Shtessel Y., Shkolnikov I., Integrated guidance and control of advanced interceptors using second order sliding modes, The 42 nd IEEE Conf on Decision and Control, pp. 4587-4592, (2003)
  • [2] Shima T., Idan M., Golan O.M., Sliding mode control for integrated missile autopilot-guidance, AIAA J of Guidance Control and Dynamics, 29, 2, pp. 250-260, (2006)
  • [3] Shima T., Golan O.M., Bound differential games guidance law for dual-controlled missiles, IEEE J of Control Systems Technology, 14, 4, pp. 719-724, (2006)
  • [4] Shima T., Shinar J., Time varying pursuit-evasion game models with bounded control, J of Guidance, Control and Dynamics, 25, 3, pp. 425-432, (2002)
  • [5] Shima T., Golan O.M., Head pursuit guidance, J of Guidance, Control and Dynamics, 30, 5, pp. 1437-1444, (2007)
  • [6] Shima T., Golan O.M., Linear quadratic differential games guidance law for dual controlled missiles, IEEE J of Aerospace and Electronic Systems, 43, 3, pp. 834-842, (2007)
  • [7] Battistini S., Shima T., Differential games missile guidance with bearings-only measurements, IEEE J of Aerospace and Electronic Systems, 50, 4, pp. 2906-2915, (2014)
  • [8] Xin M., Balakrishnan S.N., Ohlmeyer E.J., Integratedguidance and control of missiles with _-D method, IEEE J of Control Systems Technology, 14, 6, pp. 981-992, (2006)
  • [9] Xin M., Balakrishnan S.N., Nonlinear Hinfin missile longitudinal autopilot design with _-D method, IEEE J of Aerospace and Electronic Systems, 44, 1, pp. 41-56, (2008)
  • [10] Jiang H., Zhao G.R., Zhao Z.X., Integrated guidance and control design of vehicle based on block diagonal control, Flight Dynamics, 31, 5, pp. 437-442, (2013)
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