Paper Title:
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.

  Info
Periodical
Chapter
Chapter 2: Advanced Design Science (1)
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, L. W. Jun, L. B. Tong, "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
$32.00
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