Joint Kalman Filtering and Recursive Maximum Likelihood Estimation Approaches to Fault Detection and Identification of Boeing 747 Sensors and Actuators-Reference-Cited by-同舟云学术

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Joint Kalman Filtering and Recursive Maximum Likelihood Estimation Approaches to Fault Detection and Identification of Boeing 747 Sensors and Actuators

Published:2013-01-05 Issue: Volume: Page:
ISSN:
Container-title:51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
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Author:

Amirarfaei Faegheh¹,Baniamerian Amir¹,Khorasani K.¹

Affiliation:

1. Concordia University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-580

Reference17 articles.

1. Bibliographical review on reconfigurable fault-tolerant control systems

2. Fault tolerant control using augmented fault detection filter

3. Design of integrated fault detection, diagnosis and reconfigurable control systems

4. A survey of design methods for failure detection in dynamic systems

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1. Enhancing the Performance of the Photovoltaic Cells Employing Computer Vision;2023 IEEE International Workshop on Metrology for Living Environment (MetroLivEnv);2023-05-29

2. On Hybrid Health Monitoring of Photovoltaics;2022 International Conference on Electrical and Computing Technologies and Applications (ICECTA);2022-11-23

3. In-the-Loop Simulation Experiment of Aero-Engine Fault-Tolerant Control Technology;Applied Sciences;2022-02-07

4. Recursive Actuator Fault Detection and Diagnosis for Emergency Landing of UASs;IFAC Proceedings Volumes;2014

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