A distributed unmanned aerial platform and launch method applied to ballistic launch

Abstract

The invention relates to a distributed unmanned flying platform and a launching method applied to ballistic launching. Two mission planes with the same structure are symmetrically arranged around the escort plane, and each mission plane is connected with the escort plane through a connecting mechanism to form a flight platform body Both the mission plane and the escort plane are tailseat unmanned aerial vehicles, two first power systems are installed on the body of the mission plane, wings are installed at both ends of the body of the mission plane, and the second power system is installed at the end of the wing ; The flight platform body completes the follow-up storage with the launch device through the tail brace, and converts the hydraulic / air pressure into mechanical kinetic energy for launch through the launch device. After reaching the predetermined height, the flight platform coordinates and turns to level flight, and the escort aircraft will transfer the resources to the mission. After the aircraft, the flight platform is separated, the escort aircraft returns, and the mission aircraft also returns after completing the task; the invention realizes the integration of storage, transportation and launch of the ballistic launch tail seat UAV, and the combined flight platform improves the effective mission load, range and take-off. stability.

Description

technical field [0001] The invention relates to a distributed unmanned aerial platform and a launching method applied to ballistic launching, and belongs to the field of aviation technology. Background technique [0002] In the horizontal flight state of the tail-sitting UAV, it flies as a conventional fixed-wing aircraft and is easy to control. In the transition flight state, the thrust is synchronously reversed relative to the airframe, and the conversion process is simplified to the maneuvering action of the fixed-wing aircraft, which is easy to operate and easy to implement. , poor maneuverability and stability. At present, the models of mature ballistic launching UAVs such as American Switchblade (Switchblade), BattleHawk (BattleHawk) individual loitering bombs, Israeli Hero 30 individual loitering bombs, Turkey's Apa Valley-II individual loitering bombs and Slovak Predator AX -1 Individual loitering missiles, rotor types include the Firefly individual loitering bomb ...

AI Technical Summary

Problems solved by technology

Although the invention provides a launching device for folding-wing drones, the type of folding-wing drones is a rotorcraft, which lacks high-speed and large-scale cruise functions after launch.

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