A Simplified Scheme for Scheduling Multivariable Controllers and its Application to a Turbofan Engine

Author:

Garg Sanjay1

Affiliation:

1. NASA Lewis Research Center, Cleveland, OH

Abstract

A simplified scheme for scheduling multivariable controllers for robust performance over a wide range of plant operating points is presented. The approach consists of scheduling only the output matrix of a dynamic controller, thus significantly reducing the number of parameters to be scheduled. Given a robust controller at a nominal design point, designed such that it gives a stable closed-loop system at various off-design operating points, the parameters of the controller output matrix are optimized such that the closed-loop response at the off-design points closely matches the design point closed-loop response. The optimization problem formulation for the synthesis of controller scheduling gains is discussed. Results are presented for controller scheduling for a turbofan engine for a conceptual Short Take-Off and Vertical Landing aircraft. The simplified controller scheduling is shown to provide satisfactory response for engine models corresponding to significant gross thrust variations from the nominal design point.

Publisher

American Society of Mechanical Engineers

Cited by 9 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. An approximate non-linear model for aeroengine control;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2011-09-16

2. Approximate Nonlinear Modeling and Feedback Linearization Control for Aeroengines;Journal of Engineering for Gas Turbines and Power;2011-05-17

3. Switching control of thrust regulation and inlet buzz protection for ducted rocket;Acta Astronautica;2010-10

4. Multiobjective Robust Regulating and Protecting Control for Aeroengines;Journal of Engineering for Gas Turbines and Power;2009-07-13

5. Development and Validation of a Civil Aircraft Engine Simulation Model for Advanced Controller Design;Journal of Engineering for Gas Turbines and Power;2008-06-23

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