- Category:
- Other systems
- Tags:
-
- File Size:
- 7kb
- Update:
- 2019-05-08
- Downloads:
- 1 Times
- Uploaded by:
- 吴狗蛋
Description: 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.
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File list (Check if you may need any files):
| Filename | Size | Date |
|---|
| 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
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| 尾旋尾翼稳定弹的空中轨迹设计\dx3.m | 1545 | 2019-01-14
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| 尾旋尾翼稳定弹的空中轨迹设计\dxl.m | 1504 | 2019-01-10
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| 尾旋尾翼稳定弹的空中轨迹设计\dxl2.m | 140 | 2019-01-12
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| 尾旋尾翼稳定弹的空中轨迹设计\main1.m | 1103 | 2019-01-14
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| 尾旋尾翼稳定弹的空中轨迹设计\program1.m | 1139 | 2019-01-10
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| 尾旋尾翼稳定弹的空中轨迹设计\program2.m | 1690 | 2019-01-04
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| 尾旋尾翼稳定弹的空中轨迹设计\program3.m | 1408 | 2019-01-04
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| 尾旋尾翼稳定弹的空中轨迹设计\program4.m | 3004 | 2019-01-16 |
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