Unmanned platform for carrying and launching heterogeneous unmanned aerial vehicle cluster

Abstract

The invention discloses a heterogeneous unmanned aerial vehicle cluster carrying and launching unmanned platform which comprises a carrying unmanned vehicle, a rear rotor wing unmanned aerial vehicle launching assembly, an upper rotor wing unmanned aerial vehicle launching assembly, a folding wing unmanned aerial vehicle launching assembly and a front rotor wing unmanned aerial vehicle launching assembly, and the rear rotor wing unmanned aerial vehicle launching assembly, the upper rotor wing unmanned aerial vehicle launching assembly and the front rotor wing unmanned aerial vehicle launching assembly are all of drawer type structures. Comprising a storage cabin, a bearing plate, a baffle, an in-cabin sliding groove, a bearing plate sliding rail, a driving device and an electric push rod, and a folding wing unmanned aerial vehicle launching assembly comprises two rotating shaft sleeves, a support, a base, a plurality of launching cylinders, two lead screws, two lead screw frames, two sliding blocks, a servo motor and a synchronous belt. According to the unmanned aerial vehicle, the ground carrying unmanned vehicle is combined with the rotor wing unmanned aerial vehicle and the folding wing unmanned aerial vehicle, cooperative carrying launching of a heterogeneous unmanned aerial vehicle cluster is formed, the capacity of integrating reconnaissance and strike is achieved, and the unmanned aerial vehicle has the advantages of being reasonable in design, easy to operate, high in safety, high in maneuverability, capable of launching various types of unmanned aerial vehicles and the like.

Description

technical field [0001] The invention belongs to the technical field of unmanned aerial vehicles, and in particular relates to a heterogeneous unmanned aerial vehicle cluster carrying and launching unmanned platform. Background technique [0002] UAV take-off types can be divided into vertical take-off, roll-off take-off and catapult take-off. Rolling takeoff has high requirements on the site, and is not flexible enough to meet the needs of field operations. Catapult take-off and vertical take-off have low environmental requirements and can achieve long-duration, large-scale monitoring and flexible hovering tracking. The structural types of UAVs mainly include rotary-wing UAVs and folding-wing UAVs. Due to its low price, simple structure, and high cost-effectiveness, rotary-wing UAVs play an important role in battlefield situational reconnaissance operations in the military. However, rotary-wing UAVs have problems such as short battery life, fragile fuselage and sensors, an...

AI Technical Summary

Problems solved by technology

However, there is currently no technical means to effectively combine the rotor UAV and the folding-wing U

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