Mathematical model of pneumatic launch system with effect of unmanned aerial vehicle, engine and propeller characteristics
Despite significant progress in the development of modern unmanned aerial vehicles (UAVs), universal launch systems are not currently used for them. In fact, each UAV project requires its own launcher, which is inefficient in many cases. To evaluate the characteristics of UAV launchers, simple metho...
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| Autor principal: | |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
National Aerospace University «Kharkiv Aviation Institute»
2023-08-01
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| Col·lecció: | Авіаційно-космічна техніка та технологія |
| Matèries: | |
| Accés en línia: | http://nti.khai.edu/ojs/index.php/aktt/article/view/2055 |
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