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Off-equilibrium linearisation-based nonlinear control of turbojet enginese with sum-of-squares programming

Y. Tang, Y. Li, T. Cui*, Y. Zheng

*Corresponding author for this work

Research output: Journal Publications and ReviewsRGC 21 - Publication in refereed journalpeer-review

Abstract

In conventional linear parameter-varying (LPV) modelling and gain scheduling control design for turbojet engines, the linearisation is performed at a set of equilibrium points, and the validity of such LPV models is ensured near the equilibria. However, the linear model can only provide an approximate description of the engine’s state when the system operates away from equilibrium. In this paper, it is suggested that such linearisation should be carried out not only at equilibrium states but also in transient (off-equilibrium) operating regimes. This will result in a global approximation to the system states whether equilibrium or off-equilibrium. Theoretically, the transient control performance can be improved by introducing such an off-equilibrium linearisation-based control procedure. Subsequently, a gain scheduling control procedure based on off-equilibrium linearisation models is proposed by using sum-of-squares (SOS) programming, which, compared with many convex programming methods, can provide less conservative results. The resulting off-equilibrium linearisation-based nonlinear control procedure with SOS programming can capture a wide range of transient engine dynamics with better accuracy, and further achieve better control performance.

© The Author(s), 2020. Published by Cambridge University Press on behalf of Royal Aeronautical Society.
Original languageEnglish
Pages (from-to)1879-1895
JournalThe Aeronautical Journal
Volume124
Issue number1282
Online published28 Sept 2020
DOIs
Publication statusPublished - Dec 2020
Externally publishedYes

Research Keywords

  • turbojet engine
  • linearisation
  • sum-of-squares programming

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