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

摘要：

　　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.

关键词： Unmanned Aircraft Flight Control System Flight Attitude Calibration Table

作者: Hongjun Zhang Wenjun Lu Libiao Tong

作者单位: New Star Research Institute of Applied Technology, Hefei 230031, China

会议类型: 国际会议

会议名称: the Second International Conference on Frontiers of Manufacturing and Design Science(第二届制造与设计科学国际会议(ICFMD 2011))

会议地点: 台湾

会议语种:英文

页码: 764-767

在线出版日期: 2011-12-11（万方平台首次上网日期，不代表论文的发表时间）