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- W2057843418 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." @default.
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- W2057843418 date "2011-10-01" @default.
- W2057843418 modified "2023-09-25" @default.
- W2057843418 title "Design and Implementation of a Detection Device for Flight Control System in Unmanned Aerial Vehicle" @default.
- W2057843418 doi "https://doi.org/10.4028/www.scientific.net/amm.121-126.764" @default.
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