Design and Implementation of a Detection Device for Flight Control System in Unmanned Aerial Vehicle
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.
Dongye Sun, Wen-Pei Sung and Ran Chen
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