CONTROL AUGMENTATION SYSTEM DESIGN FOR THE QUAD TILT-WING UAV VIA H□‡ STRUCTURE WITH GWO
33rd International Council of the Aeronautical Sciences congress, ICAS
01.01.2022
8 pages
Aufsatz (Konferenz)
Englisch
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Design of flight control system for quad tilt-wing UAV
IEEE | 2015
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