Missile Trajectory Simulation in Vertical Plane

摘要:

文章预览

In this paper, Newton's laws of motion and momentum theorem are the theoretical basis. The equations of motion in the vertical plane are the calculation basis. In order to get the ballistic and numerical solution of motion parameters of the missile, the Runge-Kutta method and matlab are used to solve the missile Trajectory. Firstly, this paper builds the trajectory model of missile in vertical plane. Secondly, this paper chooses missile control method. Thirdly, the Runge-Kutta method and matlab are used to verify the correctness. And to further analyze the law of motion parameters changed with time.

信息:

编辑:

Abdel Hamid Ismail Mourad and József Kázmér Tar

页数:

167-171

引用:

Y. H. Li et al., "Missile Trajectory Simulation in Vertical Plane", Applied Mechanics and Materials, Vol. 527, pp. 167-171, 2014

上线时间:

February 2014

输出:

价格:

$38.00

* - 通讯作者

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[4] QiSheng Guo. System Modeling and Simulation [M]. Beijing: National Defense University Press, (2007).

[5] Xiuyun Meng. Missile Guidance and Control Systems Principles [M]. Beijing: Beijing Institute of Technology Press, (2003).

[6] Paul Zarchan. Tactical and Strategic Missile Guidance. Published by the American Institute of Aeronautics and Astronautics. Inc. (1994).