Vertical take-off and landing unmanned aerial vehicle increase lift control device and control method thereof
A technology of vertical take-off and landing and control device, which is applied to vertical take-off and landing aircraft, motor vehicles, wing adjustment and other directions, and can solve the problems of small range and low flying speed of drones.
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[0024] Such as Figure 1~4 As shown, the embodiment of the vertical take-off and landing UAV increased lift control device is provided with a pair of folding drive motors 5, a pair of foldable flaps 6, a fuel sensor 7, a cargo delivery sensor 8, and a flight control system 9.
[0025] The vertical take-off and landing UAV is provided with a pair of propeller engines 1, a wing-body fusion flight wing 2, an adjustable vertical tail 3, and a pair of adjustable horizontal tails 4; On the left and right sides of the front end, the propeller engine 1 is used to provide the pulling force required for the flight of the UAV, the wing-body fusion flight wing 2 is used to provide lift for the UAV in level flight, and the adjustable vertical tail 3 is located on the wing-body fusion flight wing 2. At the top of the rear end, a pair of adjustable horizontal tail fins 4 are arranged on the left and right sides of the rear end of the wing-body fusion flying wing 2; the left flying wing fulcr...
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