Directory: software engineering
Plat: matlab
Size: 289KB
Downloads: 342
Upload time: 2008-12-29 17:00:29
Uploader: 李恒
Description:   Using proportional navigation law, in pursuit of the three-dimensional orbit decomposition to two two-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.

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