文件名称:Missile-algorithm
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基于MATLAB导弹仿真源代码(missile simulation)
给出了比例导引法的差分方程, 采用Matlab语言, 对比例导引法的导弹理想弹道进行了三维数据仿真, 绘制出三维理想弹道。随导弹与目标参数变化情况, 对理想弹道的特性进行了分析-Missile simulation based on MATLAB source code (missile simulation)
Differential equation gives the proportional navigation law, using Matlab language, ideal ballistic missile proportional navigation law were three-dimensional simulation data and draw a three-dimensional ideal trajectory. With the missile and the target parameters, the characteristics of the ideal trajectory is analyzed
给出了比例导引法的差分方程, 采用Matlab语言, 对比例导引法的导弹理想弹道进行了三维数据仿真, 绘制出三维理想弹道。随导弹与目标参数变化情况, 对理想弹道的特性进行了分析-Missile simulation based on MATLAB source code (missile simulation)
Differential equation gives the proportional navigation law, using Matlab language, ideal ballistic missile proportional navigation law were three-dimensional simulation data and draw a three-dimensional ideal trajectory. With the missile and the target parameters, the characteristics of the ideal trajectory is analyzed
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下载文件列表
Missile algorithm/main.m
Missile algorithm/state2.m
Missile algorithm/state3.m
Missile algorithm/state4.m
Missile algorithm/state5.m
Missile algorithm
Missile algorithm/state2.m
Missile algorithm/state3.m
Missile algorithm/state4.m
Missile algorithm/state5.m
Missile algorithm
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