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Your search keyword '"Hao, Zhenyang"' showing total 44 results
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44 results on '"Hao, Zhenyang"'

8. Research on Helicopter Active Vibration Elimination Electric Actuator System Based on x‑LMS Algorithm.

Author

HAO Zhenyang, YANG Jian, ZHANG Jiawen, CAO Xin, and WANG Tao

Subjects
HELICOPTERS, ELECTRIC actuators, AERODYNAMIC load, MATHEMATICAL models, PARAMETER estimation
Abstract

Copyright of Transactions of Nanjing University of Aeronautics & Astronautics is the property of Editorial Department of Journal of Nanjing University of Aeronautics & Astronautics and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)

Published
2024
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11. Stability Analysis of Sensorless Control of High‑Speed Motor in Full‑Speed for Aircraft Electric Environment Control.

Author

HAO Zhenyang, ZHANG Ya, WANG Yuxuan, CAO Xin, and ZHANG Jiawen

Subjects
DETECTORS, ROTORS, VISCOSITY, MOTOR ability, ROBUST statistics
Abstract

Copyright of Transactions of Nanjing University of Aeronautics & Astronautics is the property of Editorial Department of Journal of Nanjing University of Aeronautics & Astronautics and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)

Published
2023
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17. Speed and Axial Position Control for a Linear-Rotary Switched Reluctance Motor With Two Radial Windings

Author

He, Zhouhui, Cao, Xin, Chen, Huateng, Deng, Zhiquan, Hao, Zhenyang, Shi, Ruijie, and Meng, Xuying

Abstract

For 6/4 linear-rotary switched reluctance motors (LRSRMs), the magnetic-flux paths of the two windings are coupled in the radial direction, thus it is difficult to design the two-winding current algorithm for the linear and rotary control simultaneously. To solve this problem and achieve linear motion and rotation at the same time, speed and axial position control method is proposed by employing the equal magnetomotive force of two windings to calculate the given currents. This control method has the advantages of simple principle, easy implementation and can realize the coordinated control of rotation and linear motion. In addition, the mathematical model of LRSRM is established to facilitate the design of current algorithm. Simulation and various experiments are completed to verify the demonstrated performance of the proposed control method.

Published
2023
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20. Research and Design of Coordinated Control Strategy for Smart Electromechanical Actuator System.

Author

HAO Zhenyang, ZHANG Qiyao, CHEN Huajie, CAO Xin, and MIAO Wei

Subjects
ELECTROMECHANICAL technology, ACTUATORS, FREQUENCY response, MIMO systems, FEEDFORWARD control systems, FLIGHT control systems
Abstract

Copyright of Transactions of Nanjing University of Aeronautics & Astronautics is the property of Editorial Department of Journal of Nanjing University of Aeronautics & Astronautics and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)

Published
2022
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36. Two Different Role Division Control Strategies for Torque and Axial Force of Conical Bearingless Switched Reluctance Motor.

Author

HAO Zhenyang, MIAO Wei, CAO Xin, and ZHANG Qiyao

Subjects
RELUCTANCE motors, MAGNETIC suspension, DEGREES of freedom, MATHEMATICAL models, TORQUE control
Abstract

Copyright of Transactions of Nanjing University of Aeronautics & Astronautics is the property of Editorial Department of Journal of Nanjing University of Aeronautics & Astronautics and its content may not be copied or emailed to multiple sites or posted to a listserv without the copyright holder's express written permission. However, users may print, download, or email articles for individual use. This abstract may be abridged. No warranty is given about the accuracy of the copy. Users should refer to the original published version of the material for the full abstract. (Copyright applies to all Abstracts.)

Published
2020
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42. Decoupling control of the dual stator-winding induction generator using SVM

Author

Hu Yuwen, Liu Lingshun, Hao Zhenyang, Huang Wenxin, Zhang Yong, and Li Yong

Subjects
Engineering, Squirrel-cage rotor, Stator, business.industry, Induction generator, AC power, law.invention, law, Control theory, Control system, Voltage regulation, business, Space vector modulation, Pulse-width modulation
Abstract

A decoupling control strategy for the dual-stator winding induction generator (DWIG) system using space vector modulation (SVM) is described in this paper. The DWIG consists of a standard squirrel-cage rotor and a stator with two sets of 3-phase star-connected windings. The power winding feeds the load with DC voltage by the diode rectifier. The control-winding is fed from a static excitation controller (SEC), through which the output voltage of power-winding is regulated. Moreover, the control-winding can be designed for higher voltage than the power-winding to reduce the SEC current. It will help to reduce the power switch loss. The model of SEC is setup, based on which a de-coupler is introduced to get the fast control of d-q currents. The SVM is incorporated to produce the PWM signals. The nodal admittance method is presented to analyze the change rule of SEC during the wide- speed-range operation. An 18 kW DWIG system is provided to demonstrate the effectiveness and robustness of the proposed control strategy. dSPACE is employed to establish the rapid control prototype for the control strategy. Simulation and experimental results prove the effectiveness and good performance of DWIG system under the proposed control strategy.

Published
2008

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