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Flight test system for flapping-wing flying robot

A flying robot and flight testing technology, which is applied in the field of flapping-wing flying robots, can solve the problems of high test cost, large impact of environmental disturbance, and high damage rate, and achieve the effects of improving test efficiency, reducing prototype damage rate, and verifying effectiveness

Active Publication Date: 2020-06-12
UNIV OF SCI & TECH BEIJING
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  • Abstract
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AI Technical Summary

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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  • Flight test system for flapping-wing flying robot
  • Flight test system for flapping-wing flying robot
  • Flight test system for flapping-wing flying robot

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Embodiment Construction

[0050] In order to make the technical problems, technical solutions and advantages to be solved by the present invention clearer, the following will describe in detail with reference to the drawings and specific embodiments.

[0051] see Figure 1 to Figure 5 , the present embodiment provides a flight test system for a flapping-wing flying robot, the purpose of which is to be able to simulate the flight state of a flapping-wing flying robot and to facilitate the measurement of dynamic characteristics during flight. It is applicable to the field of flapping-wing flying robot technology. On the one hand, the prototype of the flapping-wing flying robot can be installed on the measuring mechanism, and the aerodynamic characteristics of the flapping-wing flying robot in the simulated flight state can be collected in combination with the ATI six-dimensional force sensor in the wind tunnel environment; On the one hand, in the outdoor flight test of the flapping-wing flying robot, the...

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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...

Claims

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Application Information

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IPC IPC(8): B64F5/60G01M9/02G01M9/08
CPCB64F5/60G01M9/02G01M9/08B64U10/40B64C33/02G01M9/06B64C33/00G01M9/062G01M9/065
Inventor 贺威穆新星田淑芬付强邹尧
Owner UNIV OF SCI & TECH BEIJING
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