Improved Design of Excitation Voltage Adjustment System for Power Support Van Based on Saber Simulation

Aiming to the problems existing in the excitation voltage adjustment system of aircraft power support van such as slow dynamic response speed and the poor output voltage stability, it proposes a scheme of introducing DC supply control to the excitation voltage adjustment system in order to form a do...

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Main Authors: 王余奎, 赵徐成, 常军, 王云皓
Format: Article
Language:zho
Published: Editorial Office of Control and Information Technology 2011-01-01
Series:Kongzhi Yu Xinxi Jishu
Subjects:
Online Access:http://ctet.csrzic.com/thesisDetails#10.13889/j.issn.2095-3631.2011.03.012
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author 王余奎
赵徐成
常军
王云皓
author_facet 王余奎
赵徐成
常军
王云皓
author_sort 王余奎
collection DOAJ
description Aiming to the problems existing in the excitation voltage adjustment system of aircraft power support van such as slow dynamic response speed and the poor output voltage stability, it proposes a scheme of introducing DC supply control to the excitation voltage adjustment system in order to form a double closed loop control system. For eliminating the unstable stability of switch frequency in hysteresis current control method which may cause high harmonics of output voltage and easy-damage of power switch devices, it also proposes a scheme of variable loop width and constant frequency hysteresis current control to keep high speed response and constant switch frequency. Results of simulation and test show feasibility of the introduced scheme.
format Article
id doaj-art-743b94a5549d4c3b9f335d5fd6ea1720
institution Kabale University
issn 2096-5427
language zho
publishDate 2011-01-01
publisher Editorial Office of Control and Information Technology
record_format Article
series Kongzhi Yu Xinxi Jishu
spelling doaj-art-743b94a5549d4c3b9f335d5fd6ea17202025-08-25T06:56:24ZzhoEditorial Office of Control and Information TechnologyKongzhi Yu Xinxi Jishu2096-54272011-01-01445082337841Improved Design of Excitation Voltage Adjustment System for Power Support Van Based on Saber Simulation王余奎赵徐成常军王云皓Aiming to the problems existing in the excitation voltage adjustment system of aircraft power support van such as slow dynamic response speed and the poor output voltage stability, it proposes a scheme of introducing DC supply control to the excitation voltage adjustment system in order to form a double closed loop control system. For eliminating the unstable stability of switch frequency in hysteresis current control method which may cause high harmonics of output voltage and easy-damage of power switch devices, it also proposes a scheme of variable loop width and constant frequency hysteresis current control to keep high speed response and constant switch frequency. Results of simulation and test show feasibility of the introduced scheme.http://ctet.csrzic.com/thesisDetails#10.13889/j.issn.2095-3631.2011.03.012excitation voltage adjustmentcurrent controlhysteresis controlbandwidthdynamic response speed
spellingShingle 王余奎
赵徐成
常军
王云皓
Improved Design of Excitation Voltage Adjustment System for Power Support Van Based on Saber Simulation
Kongzhi Yu Xinxi Jishu
excitation voltage adjustment
current control
hysteresis control
bandwidth
dynamic response speed
title Improved Design of Excitation Voltage Adjustment System for Power Support Van Based on Saber Simulation
title_full Improved Design of Excitation Voltage Adjustment System for Power Support Van Based on Saber Simulation
title_fullStr Improved Design of Excitation Voltage Adjustment System for Power Support Van Based on Saber Simulation
title_full_unstemmed Improved Design of Excitation Voltage Adjustment System for Power Support Van Based on Saber Simulation
title_short Improved Design of Excitation Voltage Adjustment System for Power Support Van Based on Saber Simulation
title_sort improved design of excitation voltage adjustment system for power support van based on saber simulation
topic excitation voltage adjustment
current control
hysteresis control
bandwidth
dynamic response speed
url http://ctet.csrzic.com/thesisDetails#10.13889/j.issn.2095-3631.2011.03.012
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