paper 150305044332

Published: 2015-07-09

Rapid High-accuracy Modeling Simulation Method for Full Trajectory of the Ballistic Missile

Zengping Chen,

Zengping Chen

National University of Defense Technology, China

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Jian Chen,

Jian Chen

National University of Defense Technology, China

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Gang Li,

Gang Li

National University of Defense Technology, China

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Jianhua Wu,

Jianhua Wu

National University of Defense Technology, China

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Shiyou Xu

National University of Defense Technology, China

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Proceedings of 2015 Photonics & Electromagnetics Research Symposium, Prague, July 6 - 9，Page(s)1338-1342

Abstract

In view of the existing problems of trajectory model for ballistic missile, a method for full trajectory model of a ballistic missile over a rotating, ellipsoid earth has been developed. The method is based on the theory of minimal energy. The error of flight range is calculated with the method of Bessel’s geodetic inverse solution and fourth-order Runge-Kutta, and then corrected by dichotomy iteration. The process is repeated until the ballistic missile impacts the target location within a predefined miss distance tolerance. Simulation results show that both the speed of ballistic generation and confidence get a noticeable rise with the established trajectory model in this paper.

Citation

Zengping Chen, Jian Chen, Gang Li, Jianhua Wu, and Shiyou Xu, "Rapid High-accuracy Modeling Simulation Method for Full Trajectory of the Ballistic Missile," Proceedings of 2015 Photonics & Electromagnetics Research Symposium, Prague, July 6 - 9，Page(s)1338-1342

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