Combined type air vehicle and control method thereof
A control method and aircraft technology, applied in the field of aircraft, can solve problems such as inability to take off and land vertically, lack of high-speed cruise, and demanding take-off and landing conditions, and achieve the effect of long-distance flight
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[0043] like Figure 1-4 As shown, a composite aircraft, the body 1 of the aircraft is provided with four vertically rotatable wings 2; the fronts of the four wings are all provided with rotors 4 driven by motors 3; The working attitude of the wings includes horizontal attitude and vertical attitude; when the four wings are all in the vertical attitude; the aircraft works in the multi-rotor aircraft mode; when the four wings are in the horizontal attitude, the aircraft works in the fixed-wing in aircraft mode.
[0044] Described wing is divided into front wing and rear wing; Described body is elongated; Body front section place is provided with two front wings; Body rear section place is provided with two rear wings; Each front wing is provided with a rotor and The rotors on the two front wings rotate in opposite directions; each rear wing has a rotor and the rotors on the two rear wings rotate in opposite directions.
[0045] When the wings rotate vertically, the angle of ro...
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