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Posture-changing flying robot test bench

A flying robot and test bench technology, applied in the field of electromechanical, can solve the problems of few researches on the variable attitude flying robot and less research on the test of the variable attitude flying robot, and achieve the effects of simple use, simple structure and small size

Inactive Publication Date: 2009-10-28
SHANGHAI UNIV
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

The attitude-changing flying robot is a new type of aircraft. At present, there are not many studies on the attitude-changing flying robot, and even less research on the experiment of the attitude-changing flying robot

Method used

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  • Posture-changing flying robot test bench
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  • Posture-changing flying robot test bench

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Experimental program
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Embodiment Construction

[0021] A preferred embodiment of the present invention is described in detail as follows in conjunction with accompanying drawing: See figure 1 and Figure 5 , the test of the attitude-changing aircraft includes the mechanical clamping device and the electrical measurement and control system. The mechanical clamping device is a base 1 vertically connected to a bracket 2 through a bearing group 3; the bracket 2 is slidably connected to one end of a beam 6 through a linear sliding group 4, and the other end of the beam 6 is passed through a rotating pair 7 A clamper 5 that clamps the flying robot is connected by rotation; the electrical measurement and control system is an attitude measurement and transmission system wirelessly connected to a data reception and display storage system.

[0022] see figure 2 , the structure of the above-mentioned bearing group 3 is: in the central hole of the base 1, a rotating rod 11 with a top flange is supported by two upper and lower radial...

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Abstract

The invention relates to a test platform for a flying robot with variable attitude, which is composed of a mechanical clamping device and an electrical measurement and control system. The mechanical clamping device is mainly composed of a vertical bracket and a horizontal beam of an all-aluminum structure, and its function is to limit the attitude-changing flying robot to run on a cylindrical surface whose radius is the length of the beam and whose height is the length of the bracket. The main function of the electrical measurement and control system is that the receiving end of the wireless module receives the sensor signal sent from the sending end of the wireless module, records and saves it. The part of the internal circuit installed on the holder is mainly composed of a microprocessor, an acceleration sensor, an inclination sensor, an angular rate gyro, and a wireless module sending end. The test bench has the advantages of simple structure, small size, easy use and low cost, and is mainly suitable for ground experiments of attitude-changing aerial vehicles, and also applicable to ground tests of longitudinal dynamics of various miniature flying robots.

Description

technical field [0001] The invention relates to a test bench for an attitude-changing flying robot, which is composed of a mechanical clamping device and an electrical test control system, and is mainly used for the ground test of the attitude-changing flying robot, belonging to the field of electromechanical technology. Background technique [0002] Aircraft test is a practical means used to verify and assist design, appraise performance and test process quality in the process of aircraft development. Various experimental techniques and equipment are widely used in various engineering fields of aviation and aerospace to carry out scientific experiments, mathematical and physical simulation tests and various engineering tests to verify some new theories proposed in pre-research and design, and to explore the characteristics of aircraft. For certain characteristics, verify whether the selected scheme and design parameters are correct, check the coordination, reliability and p...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M19/00G01M99/00
Inventor 王峰蒋蓁龙利民
Owner SHANGHAI UNIV