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- W2573054914 abstract "this paper considers application of L 1 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." @default.
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- W2573054914 date "2016-08-01" @default.
- W2573054914 modified "2023-09-26" @default.
- W2573054914 title "L1adaptive output feedback controller for tilt-rotor aircraft" @default.
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- W2573054914 doi "https://doi.org/10.1109/cgncc.2016.7829184" @default.
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