Identificación de Parámetros de Desempeño de un UAV a Través de Vuelos de Prueba
The design and implementation of a autonomous navigation and control system for UAV, mandates simulating the system before in-flight testing. These simulations require a computational model of the aircraft, that can be obtained from the computation of aerodynamic parameters such as the drag polar....
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| Format: | article |
| Language: | English |
| Published: |
2018
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| Online Access: | https://knepublishing.com/index.php/KnE-Engineering/article/view/1452 http://ridda2.utp.ac.pa/handle/123456789/4341 |
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