Four rotary-wing micro air vehicles use four motors as the power unit, by adjusting the motor speed control flight of underactuated systems [. In order to achieve four-rotor autonomous vehicle autonomous flight control, preliminary design of flight control system, and use F5F100LEA single-chip as computer control unit, Proposed the flight system hardware design. Vehicle has the advantages of light weight, small size, low power consumption. After several laboratory tests, the design and reliable performance, to meet the aircraft take off, hover, landing flight mode control requirements.
Four-Rotor Autonomous Vehicle
Applied Mechanics and Materials ; 505-506 ; 286-291
2014-01-16
6 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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