A tube-type launching compound-wing unmanned aerial vehicle and a method for realizing lateral rolling operation

Abstract

The invention discloses a tube-type launching compound-wing unmanned aerial vehicle and a method for realizing lateral rolling operation, comprising a fuselage, two side wings and two tail fins, the bottom of the fuselage is provided with a lower wing storage slot, and the A rotatable lower wing is installed in the storage tank of the lower wing, and the lower wing is added to the UAV, and the propeller is installed on the side wing, which realizes the fixed-wing mode flying to the target point and then hovering, which improves the suspension. The stability of the cabin solves the technical problem that the tube-type launching UAV cannot hover in the prior art; in addition, the UAV makes the UAV realize Rolling action, so that when the UAV is flying in fixed-wing mode, not only the side wings can generate rolling torque to make the aircraft achieve rolling action, but also the different rotation speeds between the three propellers can also generate rolling torque to make the aircraft achieve Rolling action, increased rate of attitude change and reduced flank loads.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicle flight control, and relates to a tubular launching unmanned aerial vehicle, a folding unmanned aerial vehicle, a fixed-wing unmanned aerial vehicle, and a multi-rotor unmanned aerial vehicle, in particular to a tubular launching compound wing unmanned aerial vehicle and its realization Method for scrolling. Background technique [0002] At present, the development of UAVs on the market is very mature in terms of flight control and power drive; but on the other hand, based on the flight principles of conventional UAVs, it also shows inherent shortcomings in diversified flight tasks: multi-rotor UAVs The structure leads to low flight speed, short battery life, and slow remote response speed of the UAV. The fixed-wing structure leads to the high minimum flight speed of the UAV, which cannot be hovered for reconnaissance, and is easy to be found. The flight method is limited. The take...

AI Technical Summary

Problems solved by technology

[0004] Aiming at the deficiencies in the prior art, the purpose of the present invention is to provide a tube-type launching compound-wing unmanned aerial vehicle and a method for realizing the rolling operation, so as to solve the technical problem that the tube-type launching unmanned aerial vehicle cannot hover in the prior art

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