A Non-contact Attitude and Position Measurement System Developed for Wind Tunnel Free Flight Test

被引:0
|
作者
Fan, Litao [1 ]
Nie, Bowen [1 ]
Guo, Tianhao [1 ]
Liu, Zhonghua [1 ]
Heyu [1 ]
机构
[1] China Aerodynam Res & Dev Ctr, 6 South Section,Second Ring Rd, Mianyang, Sichuan, Peoples R China
来源
ADVANCES IN GUIDANCE, NAVIGATION AND CONTROL, VOL 2 | 2025年 / 1338卷
关键词
Low speed wind tunnel; Non-contact measurement; Free flight test; Optical measurement; Attitude determination; Position feedback; ACCURACY; PRECISION;
D O I
10.1007/978-981-96-2204-7_58
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Model attitude and position measurement technique plays a key role in the wind tunnel free flight test. At present, the pose will be determined by a vane system mounted near the nose of the model or IMU and AHRS in the model. The larger vane sensor will add the difficulty in system modelling and identification for the intrusion of the model surface flow field, and the inner sensors will occupy the limited internal space of the model, making it hard to design inertia similarity model. An motion capture system, OptiTrack, is used to measure model attitude and position. Static tests indicate that the system has position accuracy of 1 mm and angle accuracy of 0.05 degrees, and good dynamic performance meets the requirements of data sampling rate better than 100 Hz. OptiTrack system shows better robustness compared with AHRS. The position obtained by the OptiTrack system can be used for model flight around a fixed point in the wind tunnel, which lowers the test risk effectively.
引用
收藏
页码:608 / 617
页数:10
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