A PREDICTIVE PID CONTROLER DESIGN FOR AN ACTUATOR ATTACHED INSIDE A MORPHING WING
Abstract
This research presents the modeling and simulation of a model predictive current control and PID position and speed control methods for an actuator. A brushless motor is used for the actuators in the regional morphing wing to... [ view full abstract ]
This research presents the modeling and simulation of a model predictive current control and PID position and speed control methods for an actuator. A brushless motor is used for the actuators in the regional morphing wing to change the shape of a wing upper surface and improve the laminar flow performance. For the first time, there are two methods used to control the BLDC motors for the morphing wing technology: one is a predictive controller for current control, another one is a PID controller for position and speed control. The simulation results are carried with MATLAB/SIMULINK software. Especially, in this paper, the predictive current controlling method with error squared will be proposed and tested. The approach will give us another promising approach in controlling miniature motors and the morphing wing technology, where the requirement of easy implementation and effectiveness is put together and being the first priority.
Authors
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Duc-Hien Nguyen
(École de Technologie Supérieure)
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Shehryar Khan
(École de Technologie Supérieure)
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Michel Joel Tchatchueng Kammegne
(École de Technologie Supérieure)
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Ruxandra Botez
(ETS, Laboratory of Applied Research in Active controls, Avionics and AeroServoElasticity)
Topic Areas
Topics: Integrated product development , Topics: Innovative and unconventional aircraft , Topics: Design automation and optimization , Topics: Aircraft systems and testing (non-propulsion)
Session
ADD-3 » Stability and Controls (10:30am - Wednesday, 20th May, Room Hochelaga 4)
Paper
213_Nguyen_AERO2015.pdf