L1 Adaptive Control for Aircraft Air Management System Pressure-Regulating Bleed Valve-Reference-Cited by-同舟云学术

L1 Adaptive Control for Aircraft Air Management System Pressure-Regulating Bleed Valve

Published:2017-08-10 Issue:12 Volume:139 Page:
ISSN:0022-0434
Container-title:Journal of Dynamic Systems, Measurement, and Control
language:en
Short-container-title:

Author:

Cooper John¹,Cao Chengyu¹,Tang Jiong²

Affiliation:

1. Department of Mechanical Engineering, University of Connecticut, Storrs, CT 06269 e-mail:

2. Professor Department of Mechanical Engineering, University of Connecticut, Storrs, CT 06269 e-mail:

Abstract

This paper presents an L1 adaptive controller for pressure control using an engine bleed valve in an aircraft air management system (AMS). The air management system is composed of two pressure-regulating bleed valves, a temperature control valve, a flow control valve, and a heat exchanger/precooler. Valve hysteresis due to backlash and dry friction is included in the system model. The nonlinearities involved in the system cause oscillations under linear controllers, which decrease component life. This paper is the unique in the consideration of these uncertainties for control design. This paper presents simulation results using the adaptive controller and compares them to those using a proportional–integral (PI) controller.

Publisher

ASME International

Subject

Computer Science Applications,Mechanical Engineering,Instrumentation,Information Systems,Control and Systems Engineering

Link

http://asmedigitalcollection.asme.org/dynamicsystems/article-pdf/doi/10.1115/1.4036949/6124686/ds_139_12_121005.pdf

Reference25 articles.

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2. Shang, L., and Liu, G., 2007, “Optimal Control of a Bleed Air Temperature Regulation System,” IEEE International Conference on Mechatronics and Automation (ICMA), Harbin, China, Aug. 5–8, pp. 2610–2615.10.1109/ICMA.2007.4303968

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