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

Date: April 2,2022 |Hits: 1235 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


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.


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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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