Flight control method and system of four-rotor unmanned vehicle

Flight control method and system of four-rotor unmanned vehicle

  • CN 102,591,350 A
  • Filed: 01/06/2011
  • Published: 07/18/2012
  • Est. Priority Date: 01/06/2011
  • Status: Active Application
First Claim
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1. the flight control method of four rotor unmanned vehicles is characterized in that, said flight control method comprises:

  • A) navigation elements obtains the current flight data according to aircraft current flight state;

    B) the flight control unit generates four rotary speed informations controlling four rotors respectively according to said flying quality, the remote signal of ground control station transmission or the navigation information that prestores;

    C) Motorized drive unit is adjusted the rotating speed of four rotors respectively, the controlling aircraft attitude according to said four rotary speed informations.

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