The air trajectory design of the stabilized missile with tail rotor can be realized, and the data of deflection angle, attack angle and angular velocity can be obtained.

Filename	Size	Update
尾旋尾翼稳定弹的空中轨迹设计	0	2019-05-08
尾旋尾翼稳定弹的空中轨迹设计\RBDyDt1.m	2170	2019-01-16
尾旋尾翼稳定弹的空中轨迹设计\dx3.m	1545	2019-01-14
尾旋尾翼稳定弹的空中轨迹设计\dxl.m	1504	2019-01-10
尾旋尾翼稳定弹的空中轨迹设计\dxl2.m	140	2019-01-12
尾旋尾翼稳定弹的空中轨迹设计\main1.m	1103	2019-01-14
尾旋尾翼稳定弹的空中轨迹设计\program1.m	1139	2019-01-10
尾旋尾翼稳定弹的空中轨迹设计\program2.m	1690	2019-01-04
尾旋尾翼稳定弹的空中轨迹设计\program3.m	1408	2019-01-04
尾旋尾翼稳定弹的空中轨迹设计\program4.m	3004	2019-01-16

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