Design and Implementation of a Detection Device for Flight Control System in Unmanned Aerial Vehicle

Abstract:

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Flight control system (FCS) is the command center for the unmanned aerial vehicle (UAV). A low-cost, high-precision micro-UAV attitude calibration table is designed by utilizing the structure of the vertical gyroscope of the flight attitude angle sensor. The detection device for the UAV FCS developed by loop-in-simulation achieves unmanned attitude calibration and overall performance detection of the FCS.

Info:

Periodical:

Edited by:

Dongye Sun, Wen-Pei Sung and Ran Chen

Pages:

764-767

DOI:

10.4028/www.scientific.net/AMM.121-126.764

Citation:

H. J. Zhang et al., "Design and Implementation of a Detection Device for Flight Control System in Unmanned Aerial Vehicle", Applied Mechanics and Materials, Vols. 121-126, pp. 764-767, 2012

Online since:

October 2011

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Price:

$35.00

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