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- W2327299810 abstract "In this paper, an adaptive linearization-based control design method is studied for a nonlinear aircraft flight control system model. An adaptive linear quadratic (LQ)-based control scheme is designed for the linearized models of the aircraft dynamics. To ensure the controllability of the estimated aircraft models, a parameter projection algorithm is derived for multivariable parameter estimation models. To support the use of a linearizationbased control design, the stabilizability of the nonlinear system and linearized system models is studied, to establish their inherent connection. The adaptive control algorithm is simulated on linearized lateral models of the NASA Generic Transport Model (GTM) trimmed at certain operating conditions, to verify its desired adaptation properties in handling parameter uncertainties. It is then tested on the nonlinear GTM simulink model, to show its desirable performance in dealing with uncertainties of the nonlinear aircraft system dynamics." @default.
- W2327299810 created "2016-06-24" @default.
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- W2327299810 date "2010-06-26" @default.
- W2327299810 modified "2023-10-16" @default.
- W2327299810 title "An Adaptive LQ-Based Control Design with Parameter Projection Applied to the NASA GTM" @default.
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- W2327299810 doi "https://doi.org/10.2514/6.2010-7689" @default.
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