Application of a New Fault Detection Approach to Aerocraft's Closed-Loop Control System

  • Authors:
  • Jing Zhou;Xinhan Huang

  • Affiliations:
  • Department of Control Science and Engineering, Huazhong University of Science and Technology, and Department of Mathematics and computer science, Jianghan University, Wuhan Hubei, China 430074;Department of Control Science and Engineering, Huazhong University of Science and Technology,

  • Venue:
  • ICIRA '08 Proceedings of the First International Conference on Intelligent Robotics and Applications: Part II
  • Year:
  • 2008

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Abstract

The main contributions of this paper is the successful application in the aerocraft's closed-loop control system. As we know, the fault detection approaches proposed before mainly aim at the open-loop system. Meanwhile, a new LMI (linear matrix inequality)-based filter design methodology for fault detection in LTI plants is presented. For fault detection, H ∞ and H- index are used to measure the residual's robustness against disturbances and sensitivity to faults respectively. In this paper, the H- index is transformed to H ∞ norm by using the residual error instead of residual. Eventually, the design scheme is applied in an aerocraft's longitudinal closed-loop system and the advantages of this approach are highlighted.