LPV detection filter design for Boeing 747-100/200

István Szászi, Andrés Marcos, Gary J. Balas, József Bokor

Research output: Chapter in Book/Report/Conference proceedingConference contribution

8 Citations (Scopus)

Abstract

This paper presents a fault detection and isolation (FDI) filter design using a linear parameter varying (LPV) model of the longitudinal dynamics of a Boeing 747 series 100/200. The LPV FDI filter design is based on an extension of the fundamental problem of residual generation concepts elaborated for linear, time-invariant systems. Typically, the FDI filters are designed for open-loop model, and applied in closed-loop. This paper shows the use of the LPV FDI filter for actuator failure in the closed loop LPV system and also for the situation when it is applied to the nonlinear system simulation environment representing the"true" system.

Original languageEnglish
Title of host publicationAIAA Guidance, Navigation, and Control Conference and Exhibit
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Print)9781563479786, 9781624101083
Publication statusPublished - Jan 1 2002
EventAIAA Guidance, Navigation, and Control Conference and Exhibit 2002 - Monterey, CA, United States
Duration: Aug 5 2002Aug 8 2002

Publication series

NameAIAA Guidance, Navigation, and Control Conference and Exhibit

Other

OtherAIAA Guidance, Navigation, and Control Conference and Exhibit 2002
CountryUnited States
CityMonterey, CA
Period8/5/028/8/02

ASJC Scopus subject areas

  • Aerospace Engineering
  • Control and Systems Engineering
  • Electrical and Electronic Engineering

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  • Cite this

    Szászi, I., Marcos, A., Balas, G. J., & Bokor, J. (2002). LPV detection filter design for Boeing 747-100/200. In AIAA Guidance, Navigation, and Control Conference and Exhibit (AIAA Guidance, Navigation, and Control Conference and Exhibit). American Institute of Aeronautics and Astronautics Inc..