A Two-Degrees-of-Freedom System for Wheel Traction Applications

被引：23
作者：
Roggia, Sara [1 ,2 ]
Cupertino, Francesco [3 ]
Gerada, Chris [1 ]
Galea, Michael [1 ,4 ,5 ]
机构：
[1] Univ Nottingham, Nottingham NG7 2RD, England
[2] Motor Design Ltd, Wrexham LL13 7YT, Wales
[3] Politecn Bari, Dept Elect & Informat Engn, I-70126 Bari, Italy
[4] Univ Nottingham Ningbo China, Sch Aerosp, Ningbo 315100, Zhejiang, Peoples R China
[5] Univ Nottingham Ningbo China, Inst Aerosp Technol, Ningbo 315100, Zhejiang, Peoples R China
来源：
IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS | 2018年 / 65卷 / 06期
关键词：
Axial force; conical motor; high-voltage signal injection; in-wheel actuator; more electric aircraft (MEA); sensorless control; sliding rotor; SENSORLESS VECTOR CONTROL; ELECTRIC AIRCRAFT; DESIGN; MACHINES; MOTORS;
D O I：
10.1109/TIE.2017.2767554
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
In this paper, the use of conical induction machines is proposed for an in-wheel traction application. Such machines offer a rotational movement combined with a translationalmotion of the rotor. The horizontal movement is essential when active engagement and disengagement of the motor from the wheel without any extra mechanical component is required. This paper first investigates the basic concepts of how the conical machine functions and then proposes a mission strategy for a relevant traction application. A detailed description of the full scheme is given. In order to achieve the required performance, an innovative control method for both degrees of freedom of the machine (i.e., torque production and axial movement) is proposed and validated against a small-scale demonstrator of the whole system.
引用
收藏
页码：4483 / 4491
页数：9
相关论文
共 42 条
[1]  
Agarlita SC, 2010, P INT CONF OPTIM EL, P337
[2]  
[Anonymous], 1999, P I EL ENG C EL MACH
[3]  
[Anonymous], P IEE C EL MACH SYST
[4]   Fault-Tolerant Design Considerations and Control Strategies for Aerospace Drives [J].
Bennett, John W. ;
Atkinson, Glynn J. ;
Mecrow, Barrie C. ;
Atkinson, David J. .
IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2012, 59 (05) :2049-2058
[5]  
Bitsch H., 1992, US, Patent No. [5130592 A, 5130592]
[6]  
Boldea I, 2015, 2015 INTL AEGEAN CONFERENCE ON ELECTRICAL MACHINES & POWER ELECTRONICS (ACEMP), 2015 INTL CONFERENCE ON OPTIMIZATION OF ELECTRICAL & ELECTRONIC EQUIPMENT (OPTIM) & 2015 INTL SYMPOSIUM ON ADVANCED ELECTROMECHANICAL MOTION SYSTEMS (ELECTROMOTION), P8, DOI 10.1109/OPTIM.2015.7426739
[7]  
Briz F, 2004, IEEE T IND APPL, V40, P1107, DOI [10.1109/TIA.2004.830768, 10.1109/tia.2004.830768]
[8]  
Christensen D. J., 2013, U. S. Patent, Patent No. [8 702 550 B1, 8702550]
[9]  
Cox I. W., 2012, U. S. Patent, Patent No. [8 220 740 B2, 8220740]
[10]   Multiphase Power Converter Drive for Fault-Tolerant Machine Development in Aerospace Applications [J].
de Lillo, Liliana ;
Empringham, Lee ;
Wheeler, Pat W. ;
Khwan-On, Sudarat ;
Gerada, Chris ;
Othman, M. Nazri ;
Huang, Xiaoyan .
IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2010, 57 (02) :575-583
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