Research on aero-engine analytical linearization model

Song, Hanqiang; Li, Benwei; Lin, Xianghong; Li, Jinfei

doi:10.1109/itnec.2016.7560508

Cited by 1 publication

(1 citation statement)

References 7 publications

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“…We define that (·) q represents the value of the steady‐state equilibrium point for aero‐engine. Based on the Taylor series expansion that reckons without the higher order terms above second order, a linearized model of the continuous system (70) around steady state is denoted as 46

\{\begin{cases} {\overset{x}{true}}_{c} = A_{c} x_{c} + B_{c} u_{c} \\ y_{c} = C_{c} x_{c} + D_{c} u_{c} \end{cases},

where state variable is

x_{c} = {[\begin{array}{cc} n_{L} & n_{H} \end{array}]}^{T} - {[\begin{array}{cc} n_{L} & n_{H} \end{array}]}_{q}^{T},

input variables is

u_{c} = {[\begin{array}{cc} W_{fm} & A 8 \end{array}]}^{T} - {[\begin{array}{cc} W_{fm} & A 8 \end{array}]}_{q}^{T},

output variable is

y_{c} = T_{45} - T_{45 q},

and linearized matrices are

…”

Section: Simulation Resultsmentioning

confidence: 99%

A novel linear matrix inequality‐based robust event‐triggered model predictive control for a class of discrete‐time linear systems

Ding

Peng

et al. 2021

Intl J Robust & Nonlinear

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This paper studies a linear matrix inequality (LMI)‐based robust event‐triggered model predictive control (ET‐MPC) for a class of discrete linear time‐invariant systems subject to bounded disturbances. In the presented robust event‐triggered MPC, the event‐triggered mechanism is first set by the deviation between the optimal state and actual state. In addition, the Lyapunov‐based stability condition is employed in the constraints for simplifying parameters and enhancing the universality. Subsequently, a novel design framework that involves LMIs approach is developed. In such a framework, the Lyapunov weight matrix is predesigned by solving a convex optimization problem with LMIs and the infinite horizon MPC optimization problem is also transformed as LMIs such that the computational complexity is significantly reduced. To guarantee robust constraint satisfaction, a dual‐mode control strategy is adopted. In this way, the proposed robust ET‐MPC has the ability to deal with the constrained system. Furthermore, the theoretical analysis of the recursive feasibility and stability is provided. The numerical simulations and comparison studies demonstrate that the proposed robust ET‐MPC not only has satisfying control performance but also significantly reduces the computational burden.

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