A simulator study was conducted to verify the advantages of a Newton-Raphson model-inversion technique as a design basis for an automatic trajectory control system in an aircraft with highly nonlinear characteristics. The simulation employed a detailed mathematical model of the aerodynamic and propulsion system performance characteristics of a vertical-attitude takeoff and landing tactical aircraft. The results obtained confirm satisfactory control system performance over a large portion of the flight envelope. System response to wind gusts was satisfactory for various plausible combinations of wind magnitude and direction.
Aircraft automatic flight control system with model inversion
1990-01-01
Sonstige
Keine Angabe
Englisch
Adaptive model inversion flight control for tiltrotor aircraft
Tema Archiv | 1998
|Adaptive Model Inversion Flight Control far Tiltrotor Aircraft
British Library Conference Proceedings | 1998
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