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- W2321082701 abstract "This paper investigates an integrator-backstepping control (IBSC) methodology for a strict-feedback form of nonlinear dynamic systems in the presence of model parameter errors. A systematic procedure will be addressed firstly for formulating the IBSC law for the strict-feedback model. Formulation starts with a definition of modified tracking error by adding an integral term to normal tracking error and then a recursive sequence of coordinate transformations and Lyapunov function based feedback selections results in an IBSC law to make the system well-behaved in tracking and asymptotically stable. To show the applicability, flight path angle control corresponding to the nonlinear longitudinal dynamics of F-16 aircraft model will be considered. Assumption on lift force of aircraft as a sinusoidal function of attack angle supports for simplifying the longitudinal dynamics of aircraft to the standard strict-feedback form. The control design is applied for the standard model to achieve the IBSC law for nonlinear longitudinal dynamics of aircraft. Numerical simulation will be implemented to validate and evaluate the proposed algorithm via nonlinear closed-loop system of a high performance aircraft model." @default.
- W2321082701 created "2016-06-24" @default.
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- W2321082701 date "2015-01-02" @default.
- W2321082701 modified "2023-10-01" @default.
- W2321082701 title "Integrator-Backstepping Control Design for Nonlinear Flight System Dynamics" @default.
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- W2321082701 doi "https://doi.org/10.2514/6.2015-1321" @default.
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