Analysis and design of a fixed wing unmanned aerial vehicle gas launching system
In order to meet the development requirements of unmanned aerial vehicle (UAV) boosters, a detachable launch booster for fixed wing UAVs was designed, which is driven by high-pressure carbon dioxide gas. A mathematical model for gas launch was established based on the internal ballistic equation of...
I tiakina i:
| Kaituhi matua: | |
|---|---|
| Hōputu: | Artigo |
| Reo: | Chinês |
| I whakaputaina: |
Editorial Office of Command Control and Simulation
2025-02-01
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| Rangatū: | Zhihui kongzhi yu fangzhen |
| Ngā marau: | |
| Urunga tuihono: | https://www.zhkzyfz.cn/fileup/1673-3819/PDF/1737421348761-690149133.pdf |
| Ngā Tūtohu: |
Kāore He Tūtohu, Me noho koe te mea tuatahi ki te tūtohu i tēnei pūkete!
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