Zhi-Chang Qin
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Previous Organizations / Institutes
The organizations / institutes from the scholar's other articles in the past ten years
Zhi-Chang Qin has a total of 26 co-authors. Here are the top co-authors by number of shared publications:
- Jian-Qiao Sun
Department of Mechanical Engineering, School of Engineering, University of California, Merced, USA
6 shared publications Ying Xin
5 shared publications- Furui Xiong
Science and Technology on Reactor System Design Technology Laboratory, Nuclear Power Institute of China, Chengdu 610213, China
2 shared publications - Gang Li
Michael W. Hall School of Mechanical Engineering, Mississippi State University, Starkville, MS 39762, USA
2 shared publications - Qian Ding
Department of Mechanics, Tianjin University, Tianjin, China
2 shared publications - Ying Xin
Tianjin Key Laboratory for Advanced Mechatronic System Design and Intelligent Control, School of Mechanical Engineering, Tianjin University of Technology, Tianjin 300384, China; National Demonstration Center for Experimental Mechanical and Electrical Engineering Education, Tianjin University of Technology, Tianjin 300384, China
2 shared publications
Latest Publications
- 31 July 2020
- Published by Springer Nature in Journal of Shanghai Jiaotong University (Science)
- Vol. 25 (5) , 545-552
Multi-Objective Optimal Feedback Controls for Under-Actuated Dynamical System
- 31 July 2020
- Published by Springer Nature in Journal of Shanghai Jiaotong University (Science)
- Vol. 25 (5) , 545-552
Multi-Objective Optimal Feedback Controls for Under-Actuated Dynamical System
- 11 June 2020
- Published by Springer Nature in International Journal of Dynamics and Control
- Vol. 9 (1) , 97-108
Demonstration of a model-free backstepping control on a 2-DOF laboratory helicopter
- 11 June 2020
- Published by Springer Nature in International Journal of Dynamics and Control
- Vol. 9 (1) , 97-108
Demonstration of a model-free backstepping control on a 2-DOF laboratory helicopter
- Open Access
- 19 February 2020
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Access
- Vol. 8, 36582-36594
Dual-Loop Robust Attitude Control for an Aerodynamic System With Unknown Dynamic Model: Algorithm and Experimental Validation
This paper proposes two kinds of dual-loop nonlinear robust control strategies that are implemented on an open-loop unstable two-degree-of-freedom (2-DOF) helicopter system with unmodeled dynamics and uncertainties. The inner feedback loop is considered as a nominal controller realized by an existing “intelligent” proportional differential controller (iPD) while the outer layer feedback control is regarded as a compensation loop. We study two different forms of outer loop in this paper. One is model-free sliding mode compensator (MFSMC) and another is model-free data-driven compensator (MFDDC). The combination of the shared inner loop and either of the outer loops forms two different kinds of model-free robust control strategies, i.e., iPD-MFSMC and iPD-MFDDC. Both robust control approaches are validated experimentally on the attitude tracking control of a 2-DOF laboratory helicopter, whose control objective is to have the helicopter attitudes, i.e., pitch and yaw motions, track specified trajectories. To demonstrate the utility of the two control approaches, we compare them with linear quadratic regulator (LQR), optimal feedback linearization control (OFLC) and iPD, respectively. The extensive comparison of the simulation and experimental results shows that the dual-loop robust control approaches are quite promising in controlling the systems with unknown dynamical models.
- 19 February 2020
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Access
- Vol. 8, 36582-36594
Open AccessDual-Loop Robust Attitude Control for an Aerodynamic System With Unknown Dynamic Model: Algorithm and Experimental Validation
This paper proposes two kinds of dual-loop nonlinear robust control strategies that are implemented on an open-loop unstable two-degree-of-freedom (2-DOF) helicopter system with unmodeled dynamics and uncertainties. The inner feedback loop is considered as a nominal controller realized by an existing “intelligent” proportional differential controller (iPD) while the outer layer feedback control is regarded as a compensation loop. We study two different forms of outer loop in this paper. One is model-free sliding mode compensator (MFSMC) and another is model-free data-driven compensator (MFDDC). The combination of the shared inner loop and either of the outer loops forms two different kinds of model-free robust control strategies, i.e., iPD-MFSMC and iPD-MFDDC. Both robust control approaches are validated experimentally on the attitude tracking control of a 2-DOF laboratory helicopter, whose control objective is to have the helicopter attitudes, i.e., pitch and yaw motions, track specified trajectories. To demonstrate the utility of the two control approaches, we compare them with linear quadratic regulator (LQR), optimal feedback linearization control (OFLC) and iPD, respectively. The extensive comparison of the simulation and experimental results shows that the dual-loop robust control approaches are quite promising in controlling the systems with unknown dynamical models.
- 26 December 2019
- Published by Springer Nature in International Journal of Control, Automation, and Systems
- Vol. 18 (5) , 1202-1214
Robust Experimental Study of Data-driven Optimal Control for an Underactuated Rotary Flexible Joint
- 26 December 2019
- Published by Springer Nature in International Journal of Control, Automation, and Systems
- Vol. 18 (5) , 1202-1214
Robust Experimental Study of Data-driven Optimal Control for an Underactuated Rotary Flexible Joint
- Open Access
- 9 October 2019
- Published by MDPI AG in Applied Sciences
- Vol. 9 (20) , 4206
A Study on the Electromagnetic–Temperature Coupled Analysis Method for In-Wheel Motors
As the core component of in-wheel motor-driven electric vehicles, the in-wheel motor (IWM) directly affects the driving/braking performance of each driving wheel and the driving performance of the vehicle. The IWM operation involves a coupling of multi-fields, including the electromagnetic, temperature, flow, and mechanical fields, which influence each other. It is necessary to study coupling analysis methods to obtain accurate and consistent results. In this paper, a 15 kW in-wheel motor is taken as the research object. Based on the finite element model of the IWM, the coupling factors between the electromagnetic and temperature field, and the influence trend of coupling factors on the two fields are investigated. On this basis, considering the strong coupling factors obtained from the above analysis, the unidirectional coupling and bidirectional coupling analysis methods are used to analyze the electromagnetic–temperature characteristics of the IWM, and the comparative results between the two methods are discussed. It was found that the results showed the temperature of the IWM calculated by the bidirectional coupling method was higher than that obtained by the unidirectional coupling analysis method. The maximum temperature of stator windings calculated by bidirectional coupling was 7.1% higher than that calculated by unidirectional coupling analysis, and the effect on the relative difference of torque could reach 7.4%. Bidirectional coupling can more accurately reflect the variation of variables in the fields and the prediction of motor performance in the process of motor operation. The progress made in the electromagnetic–temperature coupled analysis method can provide a theoretical basis and useful ideas for the multi-fields coupling analysis of IWMs.
- 9 October 2019
- Published by MDPI AG in Applied Sciences
- Vol. 9 (20) , 4206
Open AccessA Study on the Electromagnetic–Temperature Coupled Analysis Method for In-Wheel Motors
As the core component of in-wheel motor-driven electric vehicles, the in-wheel motor (IWM) directly affects the driving/braking performance of each driving wheel and the driving performance of the vehicle. The IWM operation involves a coupling of multi-fields, including the electromagnetic, temperature, flow, and mechanical fields, which influence each other. It is necessary to study coupling analysis methods to obtain accurate and consistent results. In this paper, a 15 kW in-wheel motor is taken as the research object. Based on the finite element model of the IWM, the coupling factors between the electromagnetic and temperature field, and the influence trend of coupling factors on the two fields are investigated. On this basis, considering the strong coupling factors obtained from the above analysis, the unidirectional coupling and bidirectional coupling analysis methods are used to analyze the electromagnetic–temperature characteristics of the IWM, and the comparative results between the two methods are discussed. It was found that the results showed the temperature of the IWM calculated by the bidirectional coupling method was higher than that obtained by the unidirectional coupling analysis method. The maximum temperature of stator windings calculated by bidirectional coupling was 7.1% higher than that calculated by unidirectional coupling analysis, and the effect on the relative difference of torque could reach 7.4%. Bidirectional coupling can more accurately reflect the variation of variables in the fields and the prediction of motor performance in the process of motor operation. The progress made in the electromagnetic–temperature coupled analysis method can provide a theoretical basis and useful ideas for the multi-fields coupling analysis of IWMs.
- 19 February 2019
- Published by Wiley in Asian Journal of Control
- Vol. 22 (4) , 1565-1578
Multi‐objective optimal motion control of a laboratory helicopter based on parallel simple cell mapping method
- 19 February 2019
- Published by Wiley in Asian Journal of Control
- Vol. 22 (4) , 1565-1578
Multi‐objective optimal motion control of a laboratory helicopter based on parallel simple cell mapping method
- 30 September 2016
- Published by ASME International in Journal of Vibration and Acoustics
- Vol. 139 (1) , 011002
Cluster Analysis and Switching Algorithm of Multi-Objective Optimal Control Design
The multi-objective optimal control design usually generates hundreds or thousands of Pareto optimal solutions. How to assist a user to select an appropriate controller to implement is a postprocessing issue. In this paper, we develop a method of cluster analysis of the Pareto optimal designs to discover the similarity of the optimal controllers. After we identify the clusters of optimal controllers, we develop a switching strategy to select controls from different clusters to improve the performance. Numerical and experimental results show that the switching control algorithm is quite promising.
- 30 September 2016
- Published by ASME International in Journal of Vibration and Acoustics
- Vol. 139 (1) , 011002
Cluster Analysis and Switching Algorithm of Multi-Objective Optimal Control Design
The multi-objective optimal control design usually generates hundreds or thousands of Pareto optimal solutions. How to assist a user to select an appropriate controller to implement is a postprocessing issue. In this paper, we develop a method of cluster analysis of the Pareto optimal designs to discover the similarity of the optimal controllers. After we identify the clusters of optimal controllers, we develop a switching strategy to select controls from different clusters to improve the performance. Numerical and experimental results show that the switching control algorithm is quite promising.