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Observer-based Fault Tolerant Controller Design for Multi-UAV Systems

다개체 무인 항공기 시스템을 위한 관측기 기반 고장포용제어기 설계

  • 지성철 (인하대학교 전자공학부) ;
  • 이호재 (인하대학교 전자공학부) ;
  • 김도완 (한밭대학교 전기공학과)
  • Received : 2012.02.26
  • Accepted : 2012.03.27
  • Published : 2012.05.01

Abstract

In this paper, we discuss an observer-based fault tolerant controller design for the unmanned aerial vehicle (UAV) systems with exogenous disturbance. To derive robust controller design conditions, we use $H_{\infty}$ design technique. The design conditions are derived in terms of linear matrix inequalities. An illustrative example is provided to show the effectiveness of the proposed methodology.

Acknowledgement

Supported by : 한국연구재단

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  1. Static Output-Feedback-Based Robust Fault Tolerant Controller Design vol.19, pp.7, 2013, https://doi.org/10.5302/J.ICROS.2013.13.1920