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This paper introduces design of flight control system based on QFT theory. Combined non-linear dynamic inversion method with singular perturbation theory, the pseudo linear Super-maneuverable flight model is established. Aiming at the uncertain factors in non-linear dynamic modeling and definituding the range of uncertain factors and system performance requirements, the mathematical model of non-linear...
In this paper, we study adaptive control redesign problem of polynomial nonlinear systems with matching parametric uncertainties. By transforming the system into its corresponding error dynamics, we will develop an adaptive control scheme in attenuating the effect of the unknown parameters on the controlled output, which is composed of tracking errors and control efforts. To achieve better controlled...
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