Rotor Position Estimation of Brushless Synchronous Starter/Generators by Using the Main Exciter as a Position Sensor

Persistent signal injection in traditional sensorless methods leads to loss, noise, reduction of the starting torque of the main generator (MG) of the brushless synchronous starter/generator (BSSG), and complicated demodulation methods. Moreover, the reversible magnetic saliency of MG and multiple rectification modes of the rotating rectifier cause errors to most existing sensorless solutions of BSSG. To avoid these drawbacks, this paper proposes a novel method to estimate the rotor position of MG for zero- and low-speed operation. Since MG and the main exciter (ME) are mounted on the same shaft, ME is used as a position sensor, eliminating concerns of the reversible magnetic saliency of MG. With reliable indicators in all rectification modes, the position of ME is extracted from the hexagonal trajectory of the rotor current space vector of ME, which is caused by the rotating rectifier. With the estimated position of ME and signal injection into the stator of MG at standstill, the initial position of MG is detected. Then, signal injection is no longer needed and the continuous position of MG is obtained from the estimated rotation angle of ME and initial position of MG. Finally, the effectiveness of this method is verified by experiments.

[1]  Jie Li,et al.  The excitation control strategy of the three-stage synchronous machine in the start mode , 2014, 2014 IEEE Applied Power Electronics Conference and Exposition - APEC 2014.

[2]  Abolfazl Vahedi,et al.  Improved dynamic average modelling of brushless excitation system in all rectification modes , 2010 .

[3]  Ningfei Jiao,et al.  Steady-state performance evaluations of three-phase brushless asynchronous excitation system for aircraft starter/generator , 2016 .

[4]  Zhuoran Zhang,et al.  Overview and analysis of PM starter/generator for aircraft electrical power systems , 2017 .

[5]  David Uzel,et al.  Self-Sensing Control of Wound Rotor Synchronous Motor Drive for Mine Hoist , 2018, IEEE Transactions on Industrial Electronics.

[6]  Weiguo Liu,et al.  Rotor position estimation of wound-rotor synchronous starter/generator , 2018 .

[7]  Yu Jiang,et al.  Decoupling start control method for aircraft wound‐rotor synchronous starter‐generator based on main field current estimation , 2018, IET Electric Power Applications.

[8]  Huizhen Wang,et al.  A Doubly Salient Starter/Generator With Two-Section Twisted-Rotor Structure for Potential Future Aerospace Application , 2012, IEEE Transactions on Industrial Electronics.

[9]  Chris Gerada,et al.  Design and Initial Testing of a High-Speed 45-kW Switched Reluctance Drive for Aerospace Application , 2017, IEEE Transactions on Industrial Electronics.

[10]  Bon-Gwan Gu,et al.  Inductance Estimation of Electrically Excited Synchronous Motor via Polynomial Approximations by Least Square Method , 2015, IEEE Transactions on Industry Applications.

[11]  Kaushik Rajashekara,et al.  Electric Starter Generators: Their Integration into Gas Turbine Engines , 2014, IEEE Industry Applications Magazine.

[12]  Bernhard Piepenbreier,et al.  Sensorless Control of Wound Field Synchronous Machines for the Whole Speed Range , 2015 .

[13]  Dianguo Xu,et al.  Rotor Position Estimation of PMSM in Low-Speed Region and Standstill Using Zero-Voltage Vector Injection , 2018, IEEE Transactions on Power Electronics.

[14]  Zhuoran Zhang,et al.  Three-phase current injection method for mitigating turn-to-turn short-circuit fault in concentrated-winding permanent magnet aircraft starter generator , 2018 .

[15]  Antonio Griffo,et al.  Design and Characterization of a Three-Phase Brushless Exciter for Aircraft Starter/Generator , 2013, IEEE Transactions on Industry Applications.

[16]  Andrea Cavagnino,et al.  Control of Shaft-Line-Embedded Multiphase Starter/Generator for Aero-Engine , 2016, IEEE Transactions on Industrial Electronics.

[17]  Mario Pacas,et al.  Rotor position identification in synchronous machines by using the excitation machine as a sensor , 2016, 2016 IEEE Symposium on Sensorless Control for Electrical Drives (SLED).

[18]  Antonio Griffo,et al.  Sensorless starting of a wound-field synchronous starter/generator for aerospace applications , 2012, IEEE Transactions on Industrial Electronics.

[19]  S. Nishikata,et al.  Studies on a sensorless starting method for self-controlled synchronous motors without , 2009, 2009 International Conference on Electrical Machines and Systems.

[20]  Jiadan Wei,et al.  An Integrated Method for Three-Phase AC Excitation and High-Frequency Voltage Signal Injection for Sensorless Starting of Aircraft Starter/Generator , 2019, IEEE Transactions on Industrial Electronics.

[21]  Weiguo Liu,et al.  Design and Control of a Two-Phase Brushless Exciter for Aircraft Wound-Rotor Synchronous Starter/Generator in the Starting Mode , 2016, IEEE Transactions on Power Electronics.

[22]  G. Friedrich,et al.  Integrated starter generator , 2009, IEEE Industry Applications Magazine.

[23]  Stephen J. Chapman,et al.  Electric Machinery Fundamentals , 1991 .

[24]  Bulent Sarlioglu,et al.  More Electric Aircraft: Review, Challenges, and Opportunities for Commercial Transport Aircraft , 2015, IEEE Transactions on Transportation Electrification.

[25]  Vaschetto Silvio,et al.  Asymmetrical twelve-phase induction starter/generator for more electric engine in aircraft , 2016 .