An autonomous take-off control system and method for a flapping-wing aircraft

Abstract

The invention provides a flapping-wing aircraft autonomous take-off control system and method. The system includes: a remote control car, a bracket, a strain measurement device, a vehicle speed measurement device, a vehicle control board, and an airborne control board; Accurate control of speed, use the strain measuring device to measure the state of force, and use these data to accurately obtain the state information of the flapping-wing aircraft before take-off, get rid of the predicament that the traditional flapping-wing aircraft needs to be hand-held and involuntary to take off, and realize the autonomous take-off of the flapping-wing aircraft . The invention can obtain a better flying initial state of the flapping-wing aircraft; under a suitable flapping-wing frequency, the power can be reduced and the efficiency can be improved after the combination of the trolley system and the aircraft system. The auxiliary system of the invention is compact in structure, light in weight, easy to carry and easy to install, and is suitable for use in the autonomous take-off control of flapping-wing aircraft.

Description

technical field [0001] The invention belongs to the technical field of flapping-wing aircraft, and in particular relates to an autonomous take-off control system and method of the flapping-wing aircraft. Background technique [0002] In recent years, Flapping-wing aerial vehicles (Flapping-wing aerial vehicles), as a new type of bionic aircraft, are bionic robots manufactured by imitating the flight methods of insects and birds. It has low and significant advantages, and has broad application prospects in national defense, military and civilian fields. However, because the flapping wing aircraft cannot flap its wings and take off in situ like the birds in reality. Through the force analysis of the flapping-wing aircraft, the weight of the aircraft is 10mN greater than the maximum lift it can provide under static conditions, which means that it is difficult for the fuselage to take off directly from a static state on the ground to generate enough lift to achieve flight. Th...

AI Technical Summary

Problems solved by technology

[0004] The purpose of the embodiment of the present invention is to solve the problem in the prior art that the flapping-wing aircraft must rely on hand-holding to launch and give initial speed, and proposes an autonomous take-off auxiliary system and autonomous take-off control method of the flapping-wing aircraft, which can get rid of the traditional flapping-wing aircraft take-off Involuntary predicament, use the encoder to carry out precise speed control of the carrier car, use the strain measurement device to measure the force state of the flapping-wing aircraft, and use these data to accurately obtain the state information of the flapping-wing aircraft before take-off, and realize the control of the flapping-wing aircraft. Take off autonomously, so that the flapping wing aircraft can obtain a better flight initial state

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