Detailed design and control of three-phase aviation inverter

Yu Cao; Yonggang Song; Xiaobin Zhang; Weilin Li

doi:10.1109/AUS.2016.7748092

Detailed design and control of three-phase aviation inverter

Yu Cao, Yonggang Song, Xiaobin Zhang, Weilin Li

School of Automation

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

5 Scopus citations

Abstract

A new control method for three-phase-bridge inverter with improved neutral forming transformer (INFT) is presented in this paper. The controlling PWM signal is obtained by combining the switching point preset PWM and unipolar SPWM, and the fundamental and harmonic content of the controlling signal are analyzed. By analysis of the relationship of phasor voltage of neutral forming transformer, an improved neutral forming transformer with a boost function is proposed. Based on the strategies previously mentioned, the topologies and design methods of three-phase aviation inverter with high DC voltage input is given. The simulation and experimental results have confirmed the validity of the design methods.

Original language	English
Title of host publication	AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	448-453
Number of pages	6
ISBN (Electronic)	9781509010875
DOIs	https://doi.org/10.1109/AUS.2016.7748092
State	Published - 17 Nov 2016
Event	2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 - Beijing, China Duration: 10 Oct 2016 → 12 Oct 2016

Publication series

Name	AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

Conference

Conference	2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016
Country/Territory	China
City	Beijing
Period	10/10/16 → 12/10/16

Keywords

single-stage inverter
switching point preset PWM
Three-phase aviation inverter

Access to Document

10.1109/AUS.2016.7748092

Cite this

Cao, Y., Song, Y., Zhang, X., & Li, W. (2016). Detailed design and control of three-phase aviation inverter. In AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems (pp. 448-453). Article 7748092 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/AUS.2016.7748092

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title = "Detailed design and control of three-phase aviation inverter",

abstract = "A new control method for three-phase-bridge inverter with improved neutral forming transformer (INFT) is presented in this paper. The controlling PWM signal is obtained by combining the switching point preset PWM and unipolar SPWM, and the fundamental and harmonic content of the controlling signal are analyzed. By analysis of the relationship of phasor voltage of neutral forming transformer, an improved neutral forming transformer with a boost function is proposed. Based on the strategies previously mentioned, the topologies and design methods of three-phase aviation inverter with high DC voltage input is given. The simulation and experimental results have confirmed the validity of the design methods.",

keywords = "single-stage inverter, switching point preset PWM, Three-phase aviation inverter",

author = "Yu Cao and Yonggang Song and Xiaobin Zhang and Weilin Li",

note = "Publisher Copyright: {\textcopyright} 2016 IEEE.; 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016 ; Conference date: 10-10-2016 Through 12-10-2016",

year = "2016",

month = nov,

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doi = "10.1109/AUS.2016.7748092",

language = "英语",

series = "AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems",

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Cao, Y, Song, Y, Zhang, X & Li, W 2016, Detailed design and control of three-phase aviation inverter. in AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems., 7748092, AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, Institute of Electrical and Electronics Engineers Inc., pp. 448-453, 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016, Beijing, China, 10/10/16. https://doi.org/10.1109/AUS.2016.7748092

Detailed design and control of three-phase aviation inverter. / Cao, Yu; Song, Yonggang; Zhang, Xiaobin et al.
AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems. Institute of Electrical and Electronics Engineers Inc., 2016. p. 448-453 7748092 (AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Detailed design and control of three-phase aviation inverter

AU - Cao, Yu

AU - Song, Yonggang

AU - Zhang, Xiaobin

AU - Li, Weilin

PY - 2016/11/17

Y1 - 2016/11/17

N2 - A new control method for three-phase-bridge inverter with improved neutral forming transformer (INFT) is presented in this paper. The controlling PWM signal is obtained by combining the switching point preset PWM and unipolar SPWM, and the fundamental and harmonic content of the controlling signal are analyzed. By analysis of the relationship of phasor voltage of neutral forming transformer, an improved neutral forming transformer with a boost function is proposed. Based on the strategies previously mentioned, the topologies and design methods of three-phase aviation inverter with high DC voltage input is given. The simulation and experimental results have confirmed the validity of the design methods.

AB - A new control method for three-phase-bridge inverter with improved neutral forming transformer (INFT) is presented in this paper. The controlling PWM signal is obtained by combining the switching point preset PWM and unipolar SPWM, and the fundamental and harmonic content of the controlling signal are analyzed. By analysis of the relationship of phasor voltage of neutral forming transformer, an improved neutral forming transformer with a boost function is proposed. Based on the strategies previously mentioned, the topologies and design methods of three-phase aviation inverter with high DC voltage input is given. The simulation and experimental results have confirmed the validity of the design methods.

KW - single-stage inverter

KW - switching point preset PWM

KW - Three-phase aviation inverter

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DO - 10.1109/AUS.2016.7748092

M3 - 会议稿件

AN - SCOPUS:85006742001

T3 - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

SP - 448

EP - 453

BT - AUS 2016 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 2016 IEEE/CSAA International Conference on Aircraft Utility Systems, AUS 2016

Y2 - 10 October 2016 through 12 October 2016

ER -

Detailed design and control of three-phase aviation inverter

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