@inproceedings{81ae3d0f7da642538e5b73fe00ccc44d,
title = "Missile Trajectory simulation in vertical plane",
abstract = "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.",
keywords = "MATLAB programming, Runge-Kutta method, Simulation, Trajectory",
author = "Li, \{Yang Hua\} and Bo Mo and Jie Zhao",
year = "2014",
doi = "10.4028/www.scientific.net/AMM.527.167",
language = "English",
isbn = "9783038350293",
series = "Applied Mechanics and Materials",
pages = "167--171",
booktitle = "Mechatronics and Computational Mechanics II",
note = "2013 2nd International Conference on Mechatronics and Computational Mechanics, ICMCM 2013 ; Conference date: 30-12-2013 Through 31-12-2013",
}