It is challenging to control a UAV during the actuator failure because it is a highly nonlinear, coupled, underactuated system. Partial UAV control is achievable by reallocating the control signals, but control over one state has to be compromised, which would be the yaw angle for the quadrotor UAVs.
Deflecting Surface-Based Total Rotor Failure Compensation for Biplane Quadrotor
Studies in Systems, Decision and Control
24.02.2023
19 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
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