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You searched: |  Subject = PID Controller,  | 
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Design of a Testbench to Investigate Stability in the Pitch of a Tilt-Wing Uav in Hover Mode
Near East University, 2023. TJ223 .Z35 2023 NEU Grand Library[General Collection] (2)
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Design of an electrically powered dual motor Tilt-Wing UAV to investigate and develop an automated stability system for pitch and roll control in takeoff, hover and landing flight modes/
University of Kyrenia, 2023. TL685 .R83 2023 University of Kyrenia Grand Library[Reference Section] (2)
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