Jeff Pieper
Current Organizations / Institutes
The organizations/institutes from the scholar's latest article
Research Subjects
Jeff Pieper has a total of 8 co-authors. Here are the top co-authors by number of shared publications:
- Qinghong Guo
Department of Electrical and Computer Engineering, University of Calgary, Calgary, AB, Canada, T2N 1N4
3 shared publications - Chris J. B. Macnab
Department of Electrical and Computer Engineering, University of Calgary, Calgary, Canada
2 shared publications - Ayman Mohamed
Mechanical Design and Production Department, Faculty of Engineering, Cairo University 1 , Giza, Egypt
1 shared publication Chris J.B. Macnab
1 shared publication- David Howe Wood
University of Calgary, Canada
1 shared publication - Ignacio Galiano Zurbriggen
Department of Electrical and Software Engineering, University of Calgary, Calgary, Canada
1 shared publication
Latest Publications
- 26 March 2025
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Sustainable Energy
- Vol. 16 (4) , 2492-2505
Dual-Loop Geometric Control of Stator Flux for Improved LVRT Response in DFIG-Based Wind Turbine Systems
Doubly Fed Induction Generator (DFIG) based wind turbinesare particularly sensitive to grid disturbances, which has implications for overall power system stability. Grid codes require continual operation of DFIGs despite certain system disturbances. During a three-phase voltage dip, the decay of a natural flux fixed to the stator of the machine induces large voltages in the rotor windings, leading to saturation of rotor converters and potential damage to the system. This work presents a novel dual-loop state-plane based architecture to solve the stator flux transient, allowing the system to regain standard operation and power reference tracking in a fast and effective manner. An outer loop geometric controller is proposed as a framework for achieving rapid and controllable transients in the decoupled state space, and various reference geometries are considered. The proposed control structure implements a unique continuous solution for both steady state and transient operating conditions and does not require any additional hardware, switching circuits, or fault detection mechanisms. Performance-based tuning is used to determine a controller that optimizes the performance index across a variety of grid fault levels, and the resultant controller is shown to achieve rapid transient response for all fault levels, with power reference tracking achieved in under one line cycle ($\text{20}\,\text{ms}$) for even the most extreme grid faults. The proposed controller is supported by detailed mathematical analysis and validated by simulation results.
- 26 March 2025
- Published by Institute of Electrical and Electronics Engineers (IEEE) in IEEE Transactions on Sustainable Energy
- Vol. 16 (4) , 2492-2505
Dual-Loop Geometric Control of Stator Flux for Improved LVRT Response in DFIG-Based Wind Turbine Systems
Doubly Fed Induction Generator (DFIG) based wind turbinesare particularly sensitive to grid disturbances, which has implications for overall power system stability. Grid codes require continual operation of DFIGs despite certain system disturbances. During a three-phase voltage dip, the decay of a natural flux fixed to the stator of the machine induces large voltages in the rotor windings, leading to saturation of rotor converters and potential damage to the system. This work presents a novel dual-loop state-plane based architecture to solve the stator flux transient, allowing the system to regain standard operation and power reference tracking in a fast and effective manner. An outer loop geometric controller is proposed as a framework for achieving rapid and controllable transients in the decoupled state space, and various reference geometries are considered. The proposed control structure implements a unique continuous solution for both steady state and transient operating conditions and does not require any additional hardware, switching circuits, or fault detection mechanisms. Performance-based tuning is used to determine a controller that optimizes the performance index across a variety of grid fault levels, and the resultant controller is shown to achieve rapid transient response for all fault levels, with power reference tracking achieved in under one line cycle ($\text{20}\,\text{ms}$) for even the most extreme grid faults. The proposed controller is supported by detailed mathematical analysis and validated by simulation results.
- Open Access
Modeling and Control of Dynamic Stall Loads on a Smart Airfoil at Low Reynolds Number
This article describes the development and testing of a modified, semi-empirical ONERA dynamic stall model for an airfoil with a trailing edge flap—a “smart airfoil”—pitching at reduced frequencies up to 0.1. The Reynolds number is . The model reconstructs the load fluctuations associated with the shedding of multiple dynamic stall vortices (DSVs) in a time-marching solution, which makes it suitable for real-time control of a trailing edge flap (TEF). No other model captures the effect of the DSVs on the aerodynamic loads on smart airfoils. The model was refined and tuned for force measurements on a smart NACA -618 airfoil model that was pitching with an inactive TEF and was validated against the measurements when the TEF was activated. A substantial laminar separation bubble can develop on this airfoil, which is challenging for modelers of the unsteady response. A closed-loop controller was designed offline in SIMULINK, and the output of the controller was applied to the TEF in a wind tunnel. The results indicated that the model has a comparable accuracy for predicting loads with the active TEF compared to inactive TEF loads. In the fully separated flow regime, the controller performed worse when dealing with the development of the laminar separation bubble and DSVs.Open AccessModeling and Control of Dynamic Stall Loads on a Smart Airfoil at Low Reynolds Number
This article describes the development and testing of a modified, semi-empirical ONERA dynamic stall model for an airfoil with a trailing edge flap—a “smart airfoil”—pitching at reduced frequencies up to 0.1. The Reynolds number is . The model reconstructs the load fluctuations associated with the shedding of multiple dynamic stall vortices (DSVs) in a time-marching solution, which makes it suitable for real-time control of a trailing edge flap (TEF). No other model captures the effect of the DSVs on the aerodynamic loads on smart airfoils. The model was refined and tuned for force measurements on a smart NACA -618 airfoil model that was pitching with an inactive TEF and was validated against the measurements when the TEF was activated. A substantial laminar separation bubble can develop on this airfoil, which is challenging for modelers of the unsteady response. A closed-loop controller was designed offline in SIMULINK, and the output of the controller was applied to the TEF in a wind tunnel. The results indicated that the model has a comparable accuracy for predicting loads with the active TEF compared to inactive TEF loads. In the fully separated flow regime, the controller performed worse when dealing with the development of the laminar separation bubble and DSVs. - 1 January 2012
- Published by ACTA Press in International Journal of Robotics and Automation
- Vol. 27 (1)
ROBUST CONTROL OF A RIGID ARTICULATED HOPPER
- 1 January 2012
- Published by ACTA Press in International Journal of Robotics and Automation
- Vol. 27 (1)
ROBUST CONTROL OF A RIGID ARTICULATED HOPPER
- 1 September 2008
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- Vol. 307 (21582181) , 743-748
Hopping with Nearly-Passive Flight Phases
The paper presents a novel method which generates hopping gaits for an articulated single leg. Inspired by human running, the flight phase is assumed to be nearly-passive. Consequently, the initial joint velocities of the flight phase can be solved by using a static optimization procedure, provided that the boundary joint angles have been picked in advance. The two hopping phases can then be dynamically optimized, with the velocity jumps of the joints predicted by a simple collision model. The direct single shooting method solves the nonlinear constrained optimization problem. Ground reaction forces and the zero-moment-point serve as constraints. Simulation results show that the proposed approach produces energy-efficient hopping gaits.
- 1 September 2008
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- Vol. 307 (21582181) , 743-748
Hopping with Nearly-Passive Flight Phases
The paper presents a novel method which generates hopping gaits for an articulated single leg. Inspired by human running, the flight phase is assumed to be nearly-passive. Consequently, the initial joint velocities of the flight phase can be solved by using a static optimization procedure, provided that the boundary joint angles have been picked in advance. The two hopping phases can then be dynamically optimized, with the velocity jumps of the joints predicted by a simple collision model. The direct single shooting method solves the nonlinear constrained optimization problem. Ground reaction forces and the zero-moment-point serve as constraints. Simulation results show that the proposed approach produces energy-efficient hopping gaits.
- 3 July 2008
- Published by Springer Nature in Journal of Intelligent & Robotic Systems
- Vol. 53 (4) , 331-358
Hopping on Even Ground and Up Stairs with a Single Articulated Leg
- 3 July 2008
- Published by Springer Nature in Journal of Intelligent & Robotic Systems
- Vol. 53 (4) , 331-358
Hopping on Even Ground and Up Stairs with a Single Articulated Leg
- 1 January 2006
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- No. 01905848,p. 11-12
Work In Progress: A Capstone Course in Practical Control Systems through Mechatronics
Mechatronics is inherently abstract. However, the concepts and applications can lead to practical issues as in control system implementation. The mechatronics program at the University of Calgary is aiming at the intersection of practical and abstract. In a yearlong experiential learning course involving a sequence of labs, students are asked to consider issues of control saturation, tuning, bias, operating range and linearity in design of combined mechanical and control systems. Graduates of the program are uniquely trained as mechatronics engineers, different from mechanical, manufacturing, electrical or instrumentation engineers. Success can be measured by both student satisfaction, via exit surveys and course evaluations, and from career opportunities found of graduates. The latter has shown to be successful in placements ranging from research to design
- 1 January 2006
- Published by Institute of Electrical and Electronics Engineers (IEEE)
- No. 01905848,p. 11-12
Work In Progress: A Capstone Course in Practical Control Systems through Mechatronics
Mechatronics is inherently abstract. However, the concepts and applications can lead to practical issues as in control system implementation. The mechatronics program at the University of Calgary is aiming at the intersection of practical and abstract. In a yearlong experiential learning course involving a sequence of labs, students are asked to consider issues of control saturation, tuning, bias, operating range and linearity in design of combined mechanical and control systems. Graduates of the program are uniquely trained as mechatronics engineers, different from mechanical, manufacturing, electrical or instrumentation engineers. Success can be measured by both student satisfaction, via exit surveys and course evaluations, and from career opportunities found of graduates. The latter has shown to be successful in placements ranging from research to design
- 1 April 2000
- Published by Elsevier in ISA Transactions
- Vol. 39 (2) , 191-203
Controller designs for constant cutting force turning machine control
- 1 April 2000
- Published by Elsevier in ISA Transactions
- Vol. 39 (2) , 191-203
Controller designs for constant cutting force turning machine control