Control method of air-ground dual-purpose rotorcraft
A technology for rotorcraft, both land and air, applied in aircraft, rotorcraft, vehicles that can be converted into aircraft, etc., can solve the problems of ground reconnaissance robot loss, time loss, power waste, etc. Stability, the effect of increasing flight speed
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[0041] The present invention will be further described below in conjunction with accompanying drawing.
[0042] Such as figure 1 , 2 , Shown in 3 and 4, the dual-purpose rotorcraft adopted by the control method of a ground-air dual-purpose rotorcraft includes a carrier plate 19, a rotor deformation arm, a camera, a gyroscope and a controller. The rotor deformation arm includes a first deformation block 1, a second deformation block 2, a third deformation block 3, a fourth deformation block 4, a motor base 5, a dual-purpose wheel wing 6, a first bevel gear 7, a second bevel gear 8, The third bevel gear 9, the fourth bevel gear 10, the fifth bevel gear 11, the sixth bevel gear 12, the connection block 13, the first motor 14, the second motor 15, the third motor 16, the fourth motor 17 and the wheel wing motor 18.
[0043] Such as image 3 with 4 As shown, the inner ends of the first deformation block 1 and the second deformation block 2 form a first rotation pair whose comm...
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