AIRCRAFT ELECTRICAL MONITORING & FAULT DETECTION

George Kusic

2004

Abstract

Fault detection and electrical system monitoring (management) for aircraft/spacecraft dc or 400 Hz electrical systems is presented. Real-time ‘snapshot’ data is collected from current and voltage measurement transducers on radial or loop aircraft electrical system and introduced into a State Estimator. The State Estimator ‘smoothes’ the data, detects bad transducers, and calculates the best estimate of the voltage and phase angle at busses of the network, i.e., the ‘state’ of the network. Experimental results of estimation and fault detection are presented.

Paper Citation

in Harvard Style

Kusic G. (2004). AIRCRAFT ELECTRICAL MONITORING & FAULT DETECTION . In Proceedings of the First International Conference on Informatics in Control, Automation and Robotics - Volume 2: ICINCO, ISBN 972-8865-12-0, pages 133-141. DOI: 10.5220/0001125501330141

in Bibtex Style

@conference{icinco04,
author={George Kusic},
title={AIRCRAFT ELECTRICAL MONITORING & FAULT DETECTION},
booktitle={Proceedings of the First International Conference on Informatics in Control, Automation and Robotics - Volume 2: ICINCO,},
year={2004},
pages={133-141},
publisher={SciTePress},
organization={INSTICC},
doi={10.5220/0001125501330141},
isbn={972-8865-12-0},
}

in EndNote Style

TY - CONF
JO - Proceedings of the First International Conference on Informatics in Control, Automation and Robotics - Volume 2: ICINCO,
TI - AIRCRAFT ELECTRICAL MONITORING & FAULT DETECTION
SN - 972-8865-12-0
AU - Kusic G.
PY - 2004
SP - 133
EP - 141
DO - 10.5220/0001125501330141