A Sliding Mode Guidance Law for Impact Time Control with Field of View Constraint

被引：0
|
作者：
Chen S. [1 ]
Chang S. [1 ]
Wu F. [1 ]
机构：
[1] School of Energy and Power Egineering, Nanjing University of Science and Technology, Nanjing, 210094, Jiangsu
来源：
Binggong Xuebao/Acta Armamentarii | 2019年 / 40卷 / 04期
关键词：
Field-of-view angle constraint; Impact time control; Missile; Proportional navigation law; Sliding mode control;
D O I：
10.3969/j.issn.1000-1093.2019.04.013
中图分类号：
学科分类号：
摘要：
To improve the robustness and engineering adaptability of the impact time control guidance law, a nonsingular impact time control guidance law with seeker's field of view constraint is designed using sliding mode technique based on the geometrical relation of projectile interception. The stability and convergence of the proposed guidance law are proved by Lyapunov theory. The theoretically analyzed and simulated results show that, when the impact time error is zero, the proposed guidance law can evolve into a pure proportional navigation guidance law, and the required terminal acceleration of the proposed guidance law is fairly smooth, converging to zero during interception. The proposed guidance law can be used to effectively control the impact time for stationary target interception and multi-missile cooperative attack. © 2019, Editorial Board of Acta Armamentarii. All right reserved.
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收藏
页码：777 / 787
页数：10
相关论文
共 31 条
  • [1] Jeon I.S., Lee J.I., Tahk M.J., Impact-time-control guidance law for anti-ship missiles, IEEE Transactions on Control Systems Technology, 14, 2, pp. 260-266, (2006)
  • [2] Jeon I.S., Lee J.I., Homing guidance law for cooperative attack of multiple missiles, Journal of Guidance, Control, and Dynamics, 33, 1, pp. 275-280, (2010)
  • [3] Cho N.H., Kim Y.D., Modified pure proportional navigation guidance law for impact time control, Journal of Guidance, Control, and Dynamics, 39, 4, pp. 852-872, (2016)
  • [4] Jeon I.S., Lee J.I., Tahk M.J., Impact-time-control guidance with generalized proportional navigation based on nonlinear formulation, Journal of Guidance, Control, and Dynamics, 39, 8, pp. 1887-1892, (2016)
  • [5] Zhang Y.A., Wang X.L., Wu H.L., Impact time control gui-dance law with field of view constrain, Aerospace Science Technology, 39, pp. 361-369, (2014)
  • [6] Zhang Y.A., Wang X.L., Wu H.L., Impact time control guidance with field-of-view constraint accounting for uncertain system lag, Proceedings of the Institution of Mechanical Engineer, Part G: Journal of Aerospace Engineering, 230, 3, pp. 515-529, (2016)
  • [7] Yang Z., Lin D.F., Wang H., Impact time control guidance law with filed-of-view limit, Systems Engineering and Electronics, 38, 9, pp. 2122-2128, (2016)
  • [8] Ma G.X., Zhang Y.A., Impact time control guidance law with seeker field-of-view limit, Journal of Ballistics, 25, 2, pp. 6-11, (2013)
  • [9] Zhang C.Y., Song J.M., Hou B., Et al., Cooperative guidance law with impact angle and impact time constraints for networked missiles, Acta Armamentarri, 37, 3, pp. 431-438, (2016)
  • [10] Jeon I.S., Lee J.I., Impact-time-control guidance law with constraints on seeker look angle, IEEE Transactions on Aerospace and Electronic Systems, 53, 7, pp. 2621-2627, (2017)
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