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

Hong Jun Zhang; Lu Wen Jun; Li Biao Tong

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

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HomeApplied Mechanics and MaterialsApplied Mechanics and Materials Vols. 121-126Design and Implementation of a Detection Device...

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

Abstract:

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.

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Periodical:

Applied Mechanics and Materials (Volumes 121-126)

Pages:

764-767

DOI:

https://doi.org/10.4028/www.scientific.net/AMM.121-126.764

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Cite this paper

Online since:

October 2011

Authors:

Hong Jun Zhang, Lu Wen Jun, Li Biao Tong

Keywords:

Flight Attitude Calibration Table, Flight Control System, Unmanned Aircraft

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