A flight direction correction method for an unmanned aerial vehicle, a control method for an unmanned aerial vehicle, and the unmanned aerial vehicle, mainly solving the problem of a complex correction method in the prior art. The flight direction correction method for an unmanned aerial vehicle comprises: obtaining, at every interval of a predetermined time T, the position of an unmanned aerial vehicle in a straight flight path section; correcting the flight direction of the unmanned aerial vehicle according to the position of the unmanned aerial vehicle obtained at the preceding time, the position of the unmanned aerial vehicle obtained at the current time, and the ending point position of the straight flight path section where the position of the unmanned aerial vehicle at the current time is located. The flight direction correction method for an unmanned aerial vehicle determines the degree of deviation of the current position according to the position of the unmanned aerial vehicle obtained at the preceding time, the position of the unmanned aerial vehicle obtained at the current time, and the ending point position of the straight flight path section where the position of the unmanned aerial vehicle at the current time is located, and adjusts the flight direction of the unmanned aerial vehicle, correcting the flight direction by means of the unmanned aerial vehicle itself, and by way of using a two-end control method, the method being simple, and the adjustment efficiency and accuracy being high.
FLIGHT DIRECTION CORRECTION METHOD FOR UNMANNED AERIAL VEHICLE, CONTROL METHOD FOR UNMANNED AERIAL VEHICLE, AND UNMANNED AERIAL VEHICLE
07.11.2019
Patent
Elektronische Ressource
Englisch
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