Fuzzy Logic Control of Modern Aircraft Electrical Power System during Transient and Steady-State Operating Conditions

被引：0

作者：

Abdel-Fadil, Reyad ^{[1
]}

Eid, Ahmad ^{[1
]}

Abdel-Salam, Mazen ^{[1
]}

机构：

[1] Aswan Univ, Dept Elect Engn, Aswan, Egypt

来源：

2014 IEEE INTERNATIONAL CONFERENCE ON POWER ELECTRONICS, DRIVES AND ENERGY SYSTEMS (PEDES) | 2014年

关键词：

fuzzy logic control; modern aircraft; military standards; variable frequency; MEA;

D O I：

暂无

中图分类号：

TE [石油、天然气工业]; TK [能源与动力工程];

学科分类号：

0807 ; 0820 ;

摘要：

In this paper, a modern civil Aircraft Electrical Power System (AEPS) is modeled, analyzed and controlled using Fuzzy Logic Control (FLC) technique. The FLC control provides a certain behavior for the AEPS during load switching to meet the military standards of the aircraft. FLC control technique used for Generator Control Unit (GCU), AC-DC Controlled rectifier, AC-AC inverter and DC-DC Converter. With this control, the voltage at the main buses (variable frequency bus - 270VDC bus - 28VDC bus-constant frequency bus) lies within standard limits at transient and steady state conditions. At the other hand, the generator frequency lies within standard limits for all the frequency operating range of 400-800Hz. The AEPS is tested using a simulation model in PSIM and the obtained results verify that the FLC is an efficient control technique for the variable frequency aircraft systems.

引用

页数：6

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