An internal power angle control strategy for high-speed sensorless brushless DC motors

被引:0
|
作者
Tan, Bo [1 ]
Guo, Xingyuan [2 ]
Zhao, Jun [3 ]
Ding, Xiaofeng [4 ]
Fang, Wei [5 ]
机构
[1] Xian Technol Univ, Sch Elect Informat Engn, Xian 710021, Peoples R China
[2] Hebei Elect Power Co Ltd, Mkt Serv Ctr State Grid, Shijiazhuang 050021, Peoples R China
[3] Aviat Ind Corp China, Xian Aviat Inst Comp Technol, Xian 710065, Peoples R China
[4] Beihang Univ, Sch Automation Sci & Elect Engn, Beijing 100083, Peoples R China
[5] Chinese Flight Test Estab, Xian 710089, Peoples R China
基金
中国国家自然科学基金;
关键词
Back-EMF detection; Brushless DC motors; Commutation control; Electric drive; Internal power angle; BLDC MOTOR; COMPENSATION STRATEGY; COMMUTATION; PERFORMANCE; DRIVE;
D O I
10.1016/j.cja.2022.01.016
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
High-speed Brushless DC Motors (BLDCMs) usually adopt a sensorless control strategy and operate in three-phase six-state drive mode. However, the sampling errors of the rotor position and the driving method increase the Internal Power Angle (IPA), resulting in a decrease in the effi-ciency of the system. Conventional IPA reduction strategies are either sensitive to motor parame-ters, or ignore diode freewheeling during the commutation process, or require additional current sensors. In this paper, a new strategy to reduce the IPA is proposed. Firstly, a Zero-Crossing Point (ZCP) detection method for the back-EMF without filter is proposed to reduce the sampling errors of the rotor position. Secondly, the relationship between the non-energized terminal voltage and the ZCP of the corresponding back-EMF is analyzed. The non-energized terminal voltage that has completed the diode freewheeling is divided into two triangles by half of the bus voltage. When the IPA is suppressed, the areas of the two triangles are equal. Thirdly, an advanced angle for reduc-ing the IPA is obtained through a PI regulator which can eliminate the deviation between the two areas. Finally, both a simulation model and an experimental circuit are built to verify the proposed control strategy.(c) 2022 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).
引用
收藏
页码:309 / 321
页数:13
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