Flight parameter testing device of micro-miniature flapping wing air vehicle

Abstract

A flight parameter testing device of a micro-miniature flapping wing air vehicle comprises a stationary track unit, a flight parameter collecting unit and a flapping wing mechanism unit. The flight parameter testing device is simple in structure and high in automation degree, the micro-miniature flapping wing air vehicle is ingeniously and dynamically tested in the flight process, the flight parameter collecting unit and the flapping wing mechanism unit move on guide rails of the stationary track unit through a sliding table, the moving speed of the sliding table is controlled through a driving motor, in this way, flight states of the flapping wing mechanism at different wind speeds are achieved, all flight parameters of the flapping wing air vehicle can be accurately measured through a laser two-dimension scanning sensor and a six-axis force sensor, and reliable flight parameter testing data are provided for researching the flapping wing air vehicle. The laying length of the guide rails can be flexibly set, and all the flight parameters of the flapping wing mechanism at different pitch angles can be tested through replacing different wing types of wings made of different materials and adjusting the wing pitch angle of the flapping wing mechanism unit.

Description

technical field [0001] The invention belongs to the technical field of flight parameter testing, in particular to a flight parameter testing device for a miniature flapping-wing aircraft. Background technique [0002] At present, micro-aircraft can be roughly divided into three types, including rotorcraft, fixed-wing aircraft and flapping-wing aircraft. For rotorcraft and fixed-wing aircraft, due to the relatively complete development of their related technologies, they are used to test the flight parameters of the aircraft. The means are relatively complete, and the relevant test equipment is also relatively complete. However, the research on flapping-wing aircraft has only developed rapidly in recent years, and the equipment that can be used to test the flight parameters of the flapping-wing aircraft is not perfect, and there are very few relevant flight parameter test data available for reference at this stage , can not meet the research needs of the flapping-wing aircra...

AI Technical Summary

Problems solved by technology

However, the research on flapping-wing aircraft has only developed rapidly in recent years, and the equipment that can be used to test the flight parameters of the flapping-wing aircraft is not perfect, and there are very few relevant flight parameter test data available for reference at this stage , can not meet the research needs of the flapping-wing aircraft, which directly affects the development of the flapping-wing aircraft, therefore, there is an urgent need for a device that can test the flight parameters of the micro-sized flapping-wing aircraft to meet the research needs of the flapping-wing aircraft, Provide assistance for the technical development of flapping wing aircraft

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