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 ]

Authors

  1. Duc-Hien Nguyen (École de Technologie Supérieure)
  2. Shehryar Khan (École de Technologie Supérieure)
  3. Michel Joel Tchatchueng Kammegne (École de Technologie Supérieure)
  4. 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