We develop a theoretical power consumption model for multi-rotor Unmanned Aircraft Systems (UAS), estimate the model parameters, and validate it by flying an IRIS+ quadrotor UAS and measuring its energy consumption experimentally. The model is derived from the helicopter literature. Such models are required to create UAS flight planning systems.
A power consumption model for multi-rotor small unmanned aircraft systems
01.06.2017
548679 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
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