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Control Loading System for KUH SFTS
  • Control Loading System for FAA Level D Rotorcraft Simulator as Unique in Domestic
  • Certificate of Patent(Actuator for Control Loading System, 10-0989555)
  • KUH : Korea Utility Helicopter
  • SFTS : Synthetic Flight Training Simulator
Development Contents
  • Direct Drive Servo System : ±50mm Stroke
  • Force Feedback Real Time Loop
  • Mass Vibration Model : Inertia, Damping, Spring
  • 1st Flight Control Model : Position VS Force Gradient
  • 2nd Flight Control Model : Trim(Release) Actuator/Auto pilot
Development Period

2008 ~ 2012

Related Organization
  • Korea Army Nonsan Aviation School
  • Korea Aerospace Industries, LTD.(KAI)
Control Loading System for KUH SFTS Image