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Sliding Mode Reconfigurable Control for Cosmic Rays Faults in Flight Systems

[+] Author Affiliations
Azeddine Ghodbane, Maarouf Saad, Jean-François Boland, Claude Thibeault

École de Technologie Supérieure, Montreal, QC, Canada

Paper No. IMECE2014-38118, pp. V04BT04A040; 6 pages
  • ASME 2014 International Mechanical Engineering Congress and Exposition
  • Volume 4B: Dynamics, Vibration, and Control
  • Montreal, Quebec, Canada, November 14–20, 2014
  • Conference Sponsors: ASME
  • ISBN: 978-0-7918-4648-3
  • Copyright © 2014 by ASME


In this paper, a FTFC system is designed to handle a cosmic rays fault affecting actuator control signal. The geometric approach is used to design the fault diagnosis module. This module determines the gravity of the fault and calculates its parameters. Based thereon, a new reconfigurable Sliding Mode Control law is designed and applied on the longitudinal linear model of the F-16 aircraft. Simulations are performed using Matlab®/Simulink® to show the effectiveness of the proposed approach.

Copyright © 2014 by ASME
Topics: Cosmic rays , Flight



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