An unmanned aerial vehicle/unmanned aircraft system including an airframe; a plurality of rotor assemblies respectively extending from a plurality of arms connected to said airframe, said rotor assemblies each having a rotor thereon with at least one rotor blade; a landing gear extending from said airframe; and a flight controller disposed on said airframe; wherein said flight controller receives instructions for unmanned aerial vehicle/unmanned aircraft system control.
HELICOPTER WITH MULTI-ROTORS AND WIRELESS CAPABILITY
2015-08-20
Patent
Elektronische Ressource
Englisch
Prediction of Maximum Lift Capability of Helicopter Rotors
Online Contents | 2015
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