this paper considers application of L1 adaptive output feedback controller to tilt-rotor aircraft longitudinal autopilot design. The proposed adaptive controller has satisfactory performance which meets ADS-33E-PRF Military Rotorcraft handing qualities specifications in the presence of unknown time-varying nonlinearities. Simulations verify the controller.
L1 adaptive output feedback controller for tilt-rotor aircraft
2016-08-01
2511667 byte
Aufsatz (Konferenz)
Elektronische Ressource
Englisch