Abstract:
An adaptive switching controller is designed and analyzed for the longitudinal dynamics of a generic hypersonic air vehicle in the whole cruise phase rather than a trimme...Show MoreMetadata
Abstract:
An adaptive switching controller is designed and analyzed for the longitudinal dynamics of a generic hypersonic air vehicle in the whole cruise phase rather than a trimmed working condition. This model is nonlinear, multivariable and unstable. The adaptive controller presented in this paper consists of a local linearization method, an adaptive switching law and a nonlinear feedback control law. Furthermore, a theorem is obtained that the closed-loop system under the adaptive switching control is stable.
Published in: 2010 Chinese Control and Decision Conference
Date of Conference: 26-28 May 2010
Date Added to IEEE Xplore: 01 July 2010
ISBN Information: