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Palabras clave – provistas por la editorial

more electric vehicles; dissimilar redundant actuation system; NSGA-II algorithm; optimization design; electrically actuated nose wheel steering; all-electric aircraft; electromagnetic damper; electromagnetic simulation; landing gear shimmy reduction; shape control; macro-fiber composites; bending; twisting; experimental validation; control system; actuator; aerospace; electromechanical; flight control; friction; modelling; position control; preliminary design; simulation; validation; fixed-wing UAV; full-electric propulsion system; axial-flux PMSMS; fault-tolerant control; phase-to-ground short circuit; failure transient analysis; prognostics; electromechanical actuators; neural network; temperature; all-electric propulsion; electric machines; fault diagnosis; inter-turn short circuit; specification; flight analysis; dimensional analysis; vibration; multidisciplinary optimization; health monitoring; electro-mechanical actuators; testing; reliability; fault-tolerant systems; aircraft anti-skid braking system; actuator faults; reconfiguration control; linear active-disturbance rejection control; deep reinforcement learning; twin delayed deep deterministic policy gradient algorithm; active cylindrical coupler; correction coefficient; finite element method; hybrid UAV; magnetic coupler; magnetic coupling; noncontact torque transmission; mean magnetic field; wire diameter; coil; sinusoidal response; square-wave response; incremental nonlinear dynamic inversion (INDI); actuator compensation; model reduction; pseudo-control hedging (PCH); helicopter attitude control