Literature DB >> 27889134

Neural adaptive observer-based sensor and actuator fault detection in nonlinear systems: Application in UAV.

Alireza Abbaspour1, Payam Aboutalebi2, Kang K Yen3, Arman Sargolzaei4.   

Abstract

A new online detection strategy is developed to detect faults in sensors and actuators of unmanned aerial vehicle (UAV) systems. In this design, the weighting parameters of the Neural Network (NN) are updated by using the Extended Kalman Filter (EKF). Online adaptation of these weighting parameters helps to detect abrupt, intermittent, and incipient faults accurately. We apply the proposed fault detection system to a nonlinear dynamic model of the WVU YF-22 unmanned aircraft for its evaluation. The simulation results show that the new method has better performance in comparison with conventional recurrent neural network-based fault detection strategies.
Copyright © 2016 ISA. Published by Elsevier Ltd. All rights reserved.

Keywords:  Adaptive fault detection; Nonlinear dynamic model; Sensor and actuator faults; Unmanned aerial vehicle

Year:  2016        PMID: 27889134     DOI: 10.1016/j.isatra.2016.11.005

Source DB:  PubMed          Journal:  ISA Trans        ISSN: 0019-0578            Impact factor:   5.468


  4 in total

1.  Intelligent Fault Detection and Classification Based on Hybrid Deep Learning Methods for Hardware-in-the-Loop Test of Automotive Software Systems.

Authors:  Mohammad Abboush; Daniel Bamal; Christoph Knieke; Andreas Rausch
Journal:  Sensors (Basel)       Date:  2022-05-27       Impact factor: 3.847

2.  The Influence of Satellite Configuration and Fault Duration Time on the Performance of Fault Detection in GNSS/INS Integration.

Authors:  Chuang Zhang; Xiubin Zhao; Chunlei Pang; Liang Zhang; Bo Feng
Journal:  Sensors (Basel)       Date:  2019-05-09       Impact factor: 3.576

Review 3.  Distributed Multisensor Data Fusion under Unknown Correlation and Data Inconsistency.

Authors:  Muhammad Abu Bakr; Sukhan Lee
Journal:  Sensors (Basel)       Date:  2017-10-27       Impact factor: 3.576

4.  Interval Fuzzy Model for Robust Aircraft IMU Sensors Fault Detection.

Authors:  Michele Crispoltoni; Mario Luca Fravolini; Fabio Balzano; Stephane D'Urso; Marcello Rosario Napolitano
Journal:  Sensors (Basel)       Date:  2018-08-01       Impact factor: 3.576

  4 in total

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