Improvement of Wind Speed Measurement Model by Meteorological UAV and System Design

Article Preview

Abstract:

At present, the error of wind speed measurement by meteorological UAV is great, in order to solve this problem, this paper identified the major sources of error by the analysis of the wind measurement model. Found that the airspeed error caused by the aircraft acceleration for the airspeed is very small, so classic airspeed measurement calculations often ignore the impact of aircraft acceleration, but the value of wind speed is smaller, so that the error caused by aircraft acceleration relative to the wind speed cannot be ignored. Therefore, this article added aircraft acceleration to re-establish the airspeed measurement model, and got an improved wind speed of calculation model. In order to verify the model, the wind speed measurement system was been designed, the system design diagram and related data processing, solver method were presented.

You might also be interested in these eBooks

Info:

Periodical:

Advanced Materials Research (Volumes 542-543)

Pages:

591-594

Citation:

Online since:

June 2012

Export:

Price:

Permissions CCC:

Permissions PLS:

Сopyright:

© 2012 Trans Tech Publications Ltd. All Rights Reserved

Share:

Citation:

[1] Shangchun Fan, Shaojie Qiao. Detection Technology and System [M]. Beijing: Beijing University of Aeronautics and Astronautics Press, 2005.

Google Scholar

[2] Weijing Zhou. A Wind Measuring Method Based on a Mini-UAV [J]. JOURNAL OF TEST AND MEASUREMENT TECHNOLOGY, 2009, 23 (4): 297-302.

Google Scholar

[3] Yingkui He. GPS measurement techniques [M]. Chongqing: Chongqing University Press, 2010.

Google Scholar

[4] Tianwen Li. GPS principles and applications [M]. Beijing: Science Press, 2003.

Google Scholar

[5] Chenghao Wang. Aviation Instrument [M]. Beijing: Science Press, 1992.

Google Scholar

[6] Chenggong Huang. Design of Airspeed Measuring System for Small Unmanned Aerial Vehicle [J]. Computer Measurement & Control, 2009, 17 (8): 1512-1516.

Google Scholar

[7] Lijun Song. Heading and Attitude Measurement System Based on MEMS Devices [D]. Xi'an: Northwestern Polytechnical University, 2007.

Google Scholar

[8] Fuqiang Liu. Strapdown attitude-based MEMS Device Measurement System [D]. Harbin: Harbin Engineering University, 2007.

Google Scholar