Flight test system for flapping-wing flying robot

Abstract

The invention provides a flight test system for a flapping-wing flying robot. The flight test system comprises an upper computer platform, a measuring mechanism and wind tunnel equipment, wherein themeasuring mechanism is used for installing a flapping-wing flying robot prototype to be measured, and the measuring mechanism and the flapping-wing flying robot prototype are arranged in wind tunnel equipment; the measuring mechanism comprises an attitude angle controller, an airflow angle controller and a triangular bracket, wherein the airflow angle controller is installed on the triangular support, the attitude angle controller is in transmission connection with the airflow angle controller, and the flapping wing flying robot prototype is detachably connected with the attitude angle controller through a first connecting piece; and the upper computer platform is in communication connection with the measuring mechanism and the wind tunnel equipment, and is used for controlling the wind speed of the wind tunnel equipment and displaying the flight state of the flapping-wing flying robot prototype in real time. According to the invention, the dynamic characteristics of the flapping-wingflying robot can be measured and analyzed, the flying performance can be tested, and the effect of verifying the model operation effectiveness can be achieved.

Description

technical field [0001] The invention relates to the technical field of flapping-wing flying robots, in particular to a flight test system for flapping-wing flying robots. Background technique [0002] The flapping wing flying robot is a new type of aircraft that imitates the flight of birds. It can obtain the lift and forward thrust required for flight through the flapping motion of the wings. It has broad application prospects in military and civilian fields: such as low-altitude reconnaissance, Urban combat, environmental monitoring, etc. Its advantages of concealment and low energy consumption make it have important development potential in both military and civilian fields. [0003] At present, there are still many problems in the study of the aerodynamic mechanism of the flapping wing motion of the flapping wing flying robot. Compared with fixed-wing and rotary-wing aircraft, the way of generating aerodynamic force of flapping-wing flying robot is different, and its m...

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Problems solved by technology

[0005] The technical problem to be solved by the present invention is to provide a flight test system for flapping-wing flying robots to solve the lack of flight testing systems for flapping-wing flying robots on the market. The prototype test mainly depends on flight tests and is greatly affected by environmental disturbances. The problem of high test cost and high damage rate

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