Robust estimation-free prescribed performance back-stepping control of air-breathing hypersonic vehicles without affine models

Abstract

ABSTRACTThis paper investigates the design of a novel estimation-free prescribed performance non-affine control strategy for the longitudinal dynamics of an air-breathing hypersonic vehicle (AHV) via back-stepping. The proposed control scheme is capable of guaranteeing tracking errors of velocity, altitude, flight-path angle, pitch angle and pitch rate with prescribed performance. By prescribed performance, we mean that the tracking error is limited to a predefined arbitrarily small residual set, with convergence rate no less than a certain constant, exhibiting maximum overshoot less than a given value. Unlike traditional back-stepping designs, there is no need of an affine model in this paper. Moreover, both the tedious analytic and numerical computations of time derivatives of virtual control laws are completely avoided. In contrast to estimation-based strategies, the presented estimation-free controller possesses much lower computational costs, while successfully eliminating the potential problem of parameter drifting. Owing to its independence on an accurate AHV model, the studied methodology exhibits excellent robustness against system uncertainties. Finally, simulation results from a fully nonlinear model clarify and verify the design.KEYWORDS: Air-breathing hypersonic vehicle (AHV)estimation-freeprescribed performanceback-stepping AcknowledgmentsThe authors would like to express their sincere thanks to anonymous reviewers for their helpful suggestions for improving the technical note. This work was supported by the National Natural Science Foundation of China (Grants No. 61573374, 61503408).Disclosure statementNo potential conflict of interest was reported by the authors.Additional informationFundingNational Natural Science Foundation of China [grant number 61573374], [grant number 61503408].