A variable configuration UAV
A technology of unmanned aerial vehicle and configuration, applied in the field of unmanned aerial vehicles, can solve the problems of inability to achieve stable hovering, precise maneuverability, short flight range, poor task load carrying capacity, etc., and achieve rapid launch, high cruising speed, and accurate maneuvering effect
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Embodiment 1
[0023] Embodiment 1. When the rocket engine is started, the UAV obtains the maximum thrust and takes off directly from the launch pad, relying on the wings to provide lift, and the rudder surfaces of the wings and tails provide flight control capabilities to achieve high-speed cruise and long-distance delivery.
Embodiment 2
[0024] In the second embodiment, when each ducted fan is activated, eight fans are used to provide lift, and the thrust of different fans can be changed through the flight control to realize low-speed short-distance maneuvering.
[0025] Working process of the present invention:
[0026] The invention is a variable-configuration unmanned aerial vehicle. The take-off state is a fixed-wing configuration. After receiving the take-off command, the rocket engine is started, and the unmanned aerial vehicle takes off from the ejection frame and flies to the designated area. At this time, the wings provide lift. The ailerons of the aircraft provide lateral maneuverability, and the V-shaped tail rudder surface on the empennage provides longitudinal maneuverability and heading maneuverability. After approaching the designated area, the rocket engine is turned off, the drogue parachute on the multi-duct fuselage is opened, and the aircraft slows down to fly. Detach from the multi-ducted...
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