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Multi-camera dynamic calibration method for measuring model attitude angle in wind tunnel test

A technology of wind tunnel test and model attitude, which is applied in the direction of measuring device, aerodynamic test, photogrammetry/video metrology, etc. It can solve the problems of high manufacturing cost, inability to calibrate the camera position and attitude, and improve the measurement accuracy Effect

Active Publication Date: 2011-09-07
INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT
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Problems solved by technology

Its disadvantages are: the position and attitude of the camera cannot be calibrated during the operation of the wind tunnel; the manufacturing cost is high, and the coordinates of the marked points on this kind of step calibration plate are required to be very accurate

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  • Multi-camera dynamic calibration method for measuring model attitude angle in wind tunnel test
  • Multi-camera dynamic calibration method for measuring model attitude angle in wind tunnel test
  • Multi-camera dynamic calibration method for measuring model attitude angle in wind tunnel test

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Embodiment Construction

[0022] Specific embodiments of the present invention such as figure 1 with figure 2 As shown, a multi-camera dynamic calibration method for model attitude angle measurement in a wind tunnel test, the method includes the following steps:

[0023] 1) Install the camera 1 for measuring the attitude angle of the model in the wind tunnel test on the upper wall 5 of the wind tunnel test section; stick the characteristic points 7 on the wind tunnel model 2, and follow the wind tunnel model 2 under the wind tunnel test section Outside the orthographic projection area on the wall surface 4, known points 6 are glued and printed. In order to obtain better measurement results, the number of known points should be greater than or equal to five.

[0024] 2) When the wind tunnel test is not running, measure the three-dimensional coordinates of the pasted known point 6 in the wind tunnel coordinate system.

[0025] 3) According to the principle of thermal expansion and cold contraction, d...

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Abstract

The invention discloses a multi-camera dynamic calibration method for measuring model attitude angle in wind tunnel test, in which a relationship between three-dimensional coordinates of a known coordinate point and temperature change of a wind tunnel test section is established based on running temperature difference of the wind tunnel test section, thus the three-dimensional coordinates of the known coordinate point corresponding to the running temperature of the wind tunnel test section is obtained so that thermal expansion and cold contraction of the wind tunnel test section are taken into consideration when the position and the gesture of the cameras for taking every picture are calibrated; aiming at the problem that error of multi-camera photographing measurement is caused by asynchronous vibration in high-speed wind tunnel vibrating environment, the reference, which is adopted when the position and the gesture of the cameras for taking every picture are dynamically calibrated, is the known coordinate point adhered to the wind tunnel test section, as a result, the vibration during the running of the high-speed wind tunnel test section is considered so that the positions and the gestures of the cameras, derived from dynamic calibration, belong to the same wind tunnel coordinate system. The method of the invention can enhance the accuracy of measuring model attitude angle.

Description

technical field [0001] The invention relates to a method for real-time measurement of the motion attitude (angle of attack, side slip angle and roll angle) of a test model in a wind tunnel test. Background technique [0002] The attitude of the wind tunnel test model during the blowing test—the model’s angle of attack, sideslip angle, and roll angle are the basic data of the wind tunnel test. The model movement attitude data in the wind tunnel test is obtained in real time and accurately. is of great significance. But in the past, the acceleration sensor can only measure the angle of attack to measure the attitude of the model, but the sideslip angle cannot be measured because there is no gravity information. In addition, using the acceleration sensor to measure the angle of attack of the model needs to reserve a space for installing the acceleration sensor when making the model, and the application is also cumbersome. [0003] The image space geometric information of two ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01M9/02G01C11/00
Inventor 黄叙辉张征宇喻波黄诗捷王水亮
Owner INST OF HIGH SPEED AERODYNAMICS OF CHINA AERODYNAMICS RES & DEV CENT
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