现代飞机电力系统的暂态和稳态模糊控制

2014 IEEE International Conference on Power Electronics, Drives and Energy Systems (PEDES) Pub Date : 2014-12-01 DOI:10.1109/PEDES.2014.7042125

Reyad Abdel-Fadil, A. Eid, M. Abdel-Salam

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引用次数: 11

摘要

本文采用模糊逻辑控制技术对现代民用飞机电力系统(AEPS)进行建模、分析和控制。FLC控制为AEPS在载荷切换过程中提供了一定的行为，以满足飞机的军用标准。FLC控制技术用于发电机控制单元(GCU)、交直流控制整流器、交直流逆变器和DC-DC变换器。通过这种控制，在瞬态和稳态条件下，主母线(变频母线- 270vdc母线- 28VDC母线-恒频母线)的电压在标准限值内。另一方面，发电机的频率在400-800Hz的所有频率工作范围内都在标准范围内。在PSIM仿真模型中对AEPS进行了测试，结果验证了FLC是一种有效的变频飞机系统控制技术。

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Fuzzy logic control of modern aircraft electrical power system during transient and steady-state operating conditions

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.

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来源期刊

2014 IEEE International Conference on Power Electronics, Drives and Energy Systems (PEDES)

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