Abstract

This paper investigates a tracking problem for flexible air-breathing hypersonic vehicles (FAHVs) with composite disturbance. The composite disturbance produced by flexible effects, parameter uncertainties, and external interferences is modeled as a kind of unknown derivative-bounded disturbance in this paper. Then a novel composite control strategy is presented for the nonlinear FAHV model with the composite disturbance, which combines a nonlinear disturbance-observer-based compensator (NDOBC) and a dynamic-inversion-based sliding mode controller (DIBSMC). Specifically, the NDOBC is constructed to estimate and compensate for the composite disturbance, and the DIBSMC is designed to track desired trajectories of velocity and flight path angle. Moreover, the uniformly ultimate boundedness of the composite system can be guaranteed by using Lyapunov theory. Finally, simulation results on a full nonlinear model of FAHVs demonstrate that the proposed nonlinear disturbance-observer-based sliding mode controller is more effective than the traditional DIBSMC. Specifically, it is shown that the chattering of traditional DIBSMC in presence of composite disturbances can be attenuated with the NDOBC.

Highlights

  • Flight control of air-breathing hypersonic vehicles (AHVs) is very important and difficult

  • (1) The composite disturbance produced by flexible effects, parameter uncertainties, and external interferences is formulated as a kind of unknown disturbance, which is considered in the control-oriented model and estimated by a nonlinear disturbance observer

  • A nonlinear disturbance observer (NDO) based sliding mode controller (NDOBSMC) is designed for the nonlinear longitudinal model of flexible air-breathing hypersonic vehicles, and it is proved that the composite system is uniformly bounded when the controller gains and disturbance observer gains meet specified conditions

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Summary

Introduction

Flight control of air-breathing hypersonic vehicles (AHVs) is very important and difficult. It may lead to a large amount of online calculations because many coefficients have to be estimated using adaptive methods To avoid these problems, a novel nonlinear disturbanceobserver-based sliding mode control strategy was proposed to achieve control objective and attenuate the composite disturbance produced by flexible effects, parameter uncertainties, and external interferences in this paper. A novel composite control strategy, which combines a nonlinear disturbance-observer-based compensator (NDOBC) and a dynamic-inversion-based sliding mode controller (DIBSMC), is presented for the nonlinear FAHV model with composite disturbance. (2) Combining a NDOBC with a DIBSMC, a nonlinear disturbanceobserver-based sliding mode controller (NDOBSMC) is proposed to make velocity and flight-path angle track desired signals and reject the composite disturbance.

Problem Formulation
Composite Controller Design
Simulation Studies
Conclusion
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