An Analytical Design-Optimization Method for Electric Propulsion Systems of Multicopter UAVs With Desired Hovering Endurance
Multicopters are becoming increasingly important both in civil and military fields. Currently, most multicopter propulsion systems are designed by experience and trial-and-error experiments, which are costly and ineffective. This paper proposes a simple and practical method to help designers find th...
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Veröffentlicht in: | IEEE/ASME transactions on mechatronics 2019-02, Vol.24 (1), p.228-239 |
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Sprache: | eng |
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