Design and Implementation of a Detection Device for Flight Control System in Unmanned Aerial Vehicle
2011 ◽
Vol 121-126
◽
pp. 764-767
◽
Keyword(s):
Low Cost
◽
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.
2016 ◽
Vol 17
(1)
◽
pp. 120-131
◽
Keyword(s):
2020 ◽
Keyword(s):
Keyword(s):
Keyword(s):
2018 ◽
Vol 54
(2)
◽
pp. 239-247
◽
Keyword(s):
Keyword(s):