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
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