文件名称:1145455565666
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matlab file to calculate trajectory for a given missile geometry and areodynamic very useful for preliminary design
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下载文件列表
1145455565666\main.m
.............\state2.m
.............\state3.m
.............\state4.m
.............\state5.m
1145455565666
.............\state2.m
.............\state3.m
.............\state4.m
.............\state5.m
1145455565666