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Description: 采用比例导引法,把三维追击轨道分解到两个二维平面上分别导引,并充分考虑到目标的
机动性对弹道的影响,用MATLAB软件编写程序模拟出导弹实际追击的三维变轨弹道,绘制出分运动和合运动中各参数的
变化曲线。最后比较了不同的追击速度和不同的导引系数k对弹道特性的影响,考虑到导弹实际飞行时受需用法向过载的
制约,导出了导引系数k应满足的普遍公式,提出了对实战具有一定参考价值的建议。
-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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Size: 295936 |
Author: 李恒 |
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Description: MATLAB动画制作代码，含多种动作，是演示的好实例-MATLAB animation code, containing a variety of actions, is to demonstrate a good example of
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Size: 2048 |
Author: 强强 |
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