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DOI:http://dx.doi.org/10.26855/jamc.2022.03.017

Research on Powered Phase Guidance Method of Ballistic Missile Based on MPSP

Date: April 2,2022 |Hits: 595 Download PDF How to cite this paper

Xinsan Li*, Qiang Shen, Can Li, Lixin Wang

Xi’an High-tech Institution, Xi’an, Shaanxi Province, China.

*Corresponding author: Xinsan Li

Abstract

Aiming at the trajectory design of ballistic missile in the powered phase, considering the influence of time deviation at the end time, the predictive static programming (MPSP) guidance method under the condition of free end time is deduced in this paper. Aiming at the free and fixed end time. Both flight time and control quantity are closed loop. The amplitude of controls at different times can be adjusted by adjusting the weight coefficient  and weight matrix  in the performance function. The MPSP guidance method for the powered phase is simulated and analyzed to verify the effectiveness of the free end time MPSP guidance method. The deviation of the flight path angle is in the range of 0.1 deg, and the altitude deviation is in the range of 1.0 m.

References

[1] Hongyu Zhou, Xiaogang Wang, Naigang Cui. (2019). Glide trajectory optimization for hypersonic vehicles via dynamic pressure control [J]. Acta Astronautica, 2019, 164.

[2] Haibo Ji, LeiWang. (2019). Trajectory Tracking Strategy for Gliding Hypersonic Vehicle with Aileron Stuck at an Unknown Angle [J]. Journal of Beijing Institute of Technology, 2019, 28(03): 447-455.

[3] Zhao Jisong, Zhang Jianhong, Li Shuang. (2019). Rapid and High-Accuracy Approach for Hypersonic Glide Vehicle Reentry Trajectory Optimization [J]. Journal of Astronautics, 2019, 40(09): 1034-1043.

[4] Yao Zhang, Xiao Wang, Shengjing Tang. (2019). A globally fixed-time solution of distributed formation control for multiple hypersonic gliding vehicles [J]. Aerospace Science and Technology, 2019.

[5] Kun Zhao, DengQing Cao, WenHu Huang. (2018). Maneuver control of the hypersonic gliding vehicle with a scissored pair of control moment gyros [J]. Science China Technological Sciences, 2018, 61(8).

[6] Jianwen Zhu, Ruizhi He, Guojian Tang,Weimin Bao. (2018). Pendulum maneuvering strategy for hypersonic glide vehicles [J]. Elsevier Masson SAS, 2018, 78.

[7] Oza, H. B. and Padhi, R. (2012). Impact-Angle-Constrained suboptimal model predictive static programming guidance of air-to-ground missiles [J]. Journal of Guidance, Control, and Dynamics, 2012, 35(1): 153-164.

[8] Arnab Maity, Harshal B., Oza and Radhakant Padhi. (2013). Generalized model predictive static programming and its application to 3D impact angle constrained guidance of Air-to-Surface missiles [C]. 2013 American Control Conference (ACC), Washington, DC, USA, 2013: 4999-5014.

How to cite this paper

Research on Powered Phase Guidance Method of Ballistic Missile Based on MPSP

How to cite this paper: Xinsan Li, Qiang Shen, Can Li, Lixin Wang. (2022) Research on Powered Phase Guidance Method of Ballistic Missile Based on MPSP. Journal of Applied Mathematics and Computation6(1), 161-166.

DOI: http://dx.doi.org/10.26855/jamc.2022.03.017

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