Sensorless Landing Control Strategy of Bistable Permanent Magnet Actuator

被引:4
作者
Li, Bo [1 ]
Tan, Cao [1 ]
Wang, Geng [2 ]
Ge, Wenqing [1 ]
Sun, Binbin [1 ]
机构
[1] Shandong Univ Technol, Sch Transportat & Vehicle Engn, Zibo 255000, Peoples R China
[2] Dalian Univ Technol, State Key Lab Struct Anal Ind Equipment, Dalian 116024, Peoples R China
基金
中国国家自然科学基金;
关键词
ELECTROMAGNETIC VALVE-ACTUATOR; EXTENDED KALMAN FILTER; LINEAR-ACTUATOR; OBSERVER; FORCE; POSITION; DESIGN;
D O I
10.1155/2019/7652438
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Bistable permanent magnet actuator (BPMA) has been widely used in on/off application. However, the response time and landing performance of on/off actuator are contradictory. Through analyzing the landing control goal of on/off actuator and sensorless technology features of the BPMA, a new sensorless landing control strategy was proposed using armature position detection instead of real-time displacement estimation or displacement sensor. The feasibility and effectiveness of the method are verified by experiment and simulation, the operation quality of BPMA is effectively improved. The results show that the first bounce decreases by 85.7% and the second bounce is avoided when the iteration converged, compared to the condition without landing control, while the response time increased by 6.8%. Meanwhile, the landing velocity decreased more than 50% and sound intensity at different frequencies reduced more than 4dB with sensorless landing control strategy. Although in this paper the control strategy was employed to a BPMA, its structure can be used to analyze and design a wide range of on/off actuator.
引用
收藏
页数:11
相关论文
共 24 条
[1]  
Dulk I., 2013, CARPATHIAN J ELECT C, V6, P36
[2]   A sensorless method tor controlling the closure of a contactor [J].
Garcia Espinosa, Antonio ;
Riba Ruiz, Jordi-Roger ;
Alabern Morera, Xavier .
IEEE TRANSACTIONS ON MAGNETICS, 2007, 43 (10) :3896-3903
[3]   A new electromagnetic engine valve actuator with less energy consumption for variable valve timing [J].
Kim, Jinho ;
Lieu, Dennis K. .
JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY, 2007, 21 (04) :602-606
[4]   Magnetic force enhancement in a linear actuator by air-gap magnetic field distribution optimization and design [J].
Lee, Jaewook ;
Dede, Ercan M. ;
Banerjee, Debasish ;
Iizuka, Hideo .
FINITE ELEMENTS IN ANALYSIS AND DESIGN, 2012, 58 :44-52
[5]  
Liu L, 2011, P IMECHE D, DOI dolI 10. 1177/0954407011411033
[6]   AN ADAPTIVE AND OPTIMIZED SWITCHING OBSERVER FOR SENSORLESS CONTROL OF AN ELECTROMAGNETIC VALVE ACTUATOR IN CAMLESS INTERNAL COMBUSTION ENGINES [J].
Mercorelli, Paolo .
ASIAN JOURNAL OF CONTROL, 2014, 16 (04) :959-973
[7]   A Hysteresis Hybrid Extended Kalman Filter as an Observer for Sensorless Valve Control in Camless Internal Combustion Engines [J].
Mercorelli, Paolo .
IEEE TRANSACTIONS ON INDUSTRY APPLICATIONS, 2012, 48 (06) :1940-1949
[8]   A Two-Stage Augmented Extended Kalman Filter as an Observer for Sensorless Valve Control in Camless Internal Combustion Engines [J].
Mercorelli, Paolo .
IEEE TRANSACTIONS ON INDUSTRIAL ELECTRONICS, 2012, 59 (11) :4236-4247
[9]   An Antisaturating Adaptive Preaction and a Slide Surface to Achieve Soft Landing Control for Electromagnetic Actuators [J].
Mercorelli, Paolo .
IEEE-ASME TRANSACTIONS ON MECHATRONICS, 2012, 17 (01) :76-85
[10]   Actuator-based hardware-in-the-loop testing of a jet engine fuel control unit in flight conditions [J].
Montazeri-Gh, M. ;
Nasiri, M. ;
Rajabi, M. ;
Jamshidfard, M. .
SIMULATION MODELLING PRACTICE AND THEORY, 2012, 21 (01) :65-77