• Title of article

    Application of a Model-Based Fault Detection Approach on a Spacecraft

  • Author/Authors

    Alikhani, A. Aerospace Research Institute - Ministry of Science, Research and Technology, Tehran, Iran , Sharifi, Gh. Department of the Aerospace Engineering - K.N. Toosi University of Technology, Tehran, Iran

  • Pages
    8
  • From page
    19
  • To page
    26
  • Abstract
    The model-based fault detection approach is one of the software-based supervision systems monitoring. This method has a marked effect to detect components fault without demanding extra sensors to measure or add redundancy. The extended multiple model’s adaptive estimation method is an online strategy to detect and isolation failure of components. Simple implementation, fast and accurate response, compatibility with nonlinear systems, and the ability to detect different types of faults are the most important features of this method. This method is applied to the faulty spacecraft in terms of actuators and its capability is evaluated. The most probable actuator fault implemented using MATLAB/SIMULINK software. The presented approach successfully detects faulty actuators.
  • Keywords
    Fault detection , Spacecraft , model-based
  • Journal title
    International Journal of Reliability, Risk and Safety: Theory and Application
  • Serial Year
    2020
  • Record number

    2734814