Li, Xiao
(2013)
Stability Analysis and Control Design for Hybrid AC-DC More-Electric Aircraft Power Systems.
Master's Thesis, University of Pittsburgh.
(Unpublished)
Abstract
This thesis studies the stability of a more-electric aircraft (MEA) power system with hybrid converters and loads, and proposes a control design method using state feedback. The MEA is aimed to replace the conventional nonelectric power in aircraft with electric power in order to reduce the size and weight of the aircraft power system. This thesis considers a model of the MEA power system consisting of the following components: converters with uncontrolled diodes and controlled rectifiers, ideal constant power loads (CPL), and non-ideal CPL driven by electromechanical actuators. The system has narrow stability range under the conventional two-loop PI control. To improve control performance, a full-state feedback control method is developed that can significantly increase the stability margin of the MEA power system.
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Details
Item Type: |
University of Pittsburgh ETD
|
Status: |
Unpublished |
Creators/Authors: |
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ETD Committee: |
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Date: |
24 September 2013 |
Date Type: |
Publication |
Defense Date: |
1 April 2013 |
Approval Date: |
24 September 2013 |
Submission Date: |
15 June 2013 |
Access Restriction: |
No restriction; Release the ETD for access worldwide immediately. |
Number of Pages: |
56 |
Institution: |
University of Pittsburgh |
Schools and Programs: |
Swanson School of Engineering > Electrical Engineering |
Degree: |
MS - Master of Science |
Thesis Type: |
Master's Thesis |
Refereed: |
Yes |
Uncontrolled Keywords: |
MEA, power system, stability, CPL, converter,full-state feedback controll |
Date Deposited: |
24 Sep 2013 19:57 |
Last Modified: |
15 Nov 2016 14:13 |
URI: |
http://d-scholarship.pitt.edu/id/eprint/19024 |
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