Actuator failure detection and reconfigurable control for F-16 aircraft model-Reference-Cited by-同舟云学术

Actuator failure detection and reconfigurable control for F-16 aircraft model

Published:2003-06 Issue:7 Volume:36 Page:53-58
ISSN:1474-6670
Container-title:IFAC Proceedings Volumes
language:en
Short-container-title:IFAC Proceedings Volumes

Author:

Caliskan Fikret,Hajiyev Chingiz

Publisher

Elsevier BV

Subject

General Medicine

Reference9 articles.

1. Dynamic systems diagnosis based on Kalman filter updating sequences.;Gadzhiev Hajiyev);Automation and Remote Control,1992

2. Check of the generalized variance of the Kalman filter updating sequence in dynamic diagnosis.;Gadzhiev (Hajiyev);Automation and Remote Control,1994

3. The Information Provision of Offshore Platform Supervision and Control;Gadzhiev (Hajiyev),1996

4. Sensor/actuator fault diagnosis based on statistical analysis of innovation sequence and Robust Kalman Filtering,;Hajiyev;Aerospace Science and Technology,2000

5. Integrated sensor/actuator FDI and reconfigurable control for fault-tolerant flight control system design.;Hajiyev;The Aeronautical Journal,2001

Cited by 5 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Testing the Determinant of the Innovation Covariance Matrix Applied to Aircraft Sensor and Actuator/Surface Fault Detection;Advances in Sustainable Aviation;2017-11-09

2. Generalized Rayleigh quotient based innovation covariance testing applied to sensor/actuator fault detection;Measurement;2014-01

3. Aircraft Icing Detection, Identification, and Reconfigurable Control Based on Kalman Filtering and Neural Networks;Journal of Aerospace Engineering;2008-04

4. Aircraft Icing Detection, Identification and Reconfigurable Control Based on Kalman Filtering and Neural Networks;AIAA Atmospheric Flight Mechanics Conference and Exhibit;2005-06-19

5. Kalman filter and neural network‐based icing identification applied to A340 aircraft dynamics;Aircraft Engineering and Aerospace Technology;2005-02