Using proportional navigation law, in pursuit of the three-dimensional orbit decomposition to tw o-dimensional plane, respectively, guidance, and taking fully into account the objectives of the impact of mobility on the trajectory, using MATLAB software programming practical pursuit of missile simulated three-dimensional orbit trajectory , to map out points Movement Hop movement curve of each parameter. Finally, the pursuit of different speed and different-guided ballistic coefficient k on the characteristics of, taking into account the actual missile flight by the need to overload the use of constraints derived Seeker coefficient k should satisfy the general formula, put forward on the actual reference value has a certain proposal.

基于Matlab的三维动态弹道仿真研究.caj
基于Matlab的三维动态弹道仿真研究.txt

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