Mission planning strategy for multirotor UAV based on flight endurance estimation
| Autor: | C.D. García-Beltrán, Didier Theilliol, Carlos-Manuel Astorga-Zaragoza, Jean-Christophe Ponsart, R. Schacht-Rodriguez |
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| Přispěvatelé: | Centre de Recherche en Automatique de Nancy (CRAN), Université de Lorraine (UL)-Centre National de la Recherche Scientifique (CNRS), Centro Nacional de Investigación y Desarrollo Tecnológico (CENIDET) |
| Jazyk: | angličtina |
| Rok vydání: | 2019 |
| Předmět: |
Battery (electricity)
0209 industrial biotechnology Mission Planning State of health Computer science 010103 numerical & computational mathematics 02 engineering and technology Energy consumption Energy Consumption Power Supply Fault (power engineering) 01 natural sciences 7. Clean energy Automotive engineering [SPI.AUTO]Engineering Sciences [physics]/Automatic 020901 industrial engineering & automation State of charge 0101 mathematics Multirotor Actuator Energy (signal processing) Unmanned Aerial Vehicles Path Generation |
| Zdroj: | International Conference on Unmanned Aircraft Systems, ICUAS 2019 International Conference on Unmanned Aircraft Systems, ICUAS 2019, Jun 2019, Atlanta, GA, United States. pp.778-786, ⟨10.1109/ICUAS.2019.8798292⟩ |
| DOI: | 10.1109/ICUAS.2019.8798292⟩ |
| Popis: | International audience; In this paper, the impact of fault effects occurring in actuators on energy consumption for multirotor UAV during mission development is analyzed. The multirotors are typically powered by Lithium Polymer batteries where the total mission time depends on the energy available on board. According to battery and actuators health, the discharge rate tends to increase which decrease the flight endurance causing that battery to discharge completely without guaranteeing the fulfillment of the mission or even a safety landing. In that sense, a model able to determines the maximum energy and flight endurance is used considering the battery discharge, State of Charge (SoC) and State of Health (SoH) and its impact during the mission execution is evaluated considering the fault effects in actuators modeled as loss of effectiveness. The proposed approach is tested at simulation level considering an hexarotor UAV. |
| Databáze: | OpenAIRE |
| Externí odkaz: |
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