Actuator Fault Diagnosis in a Boeing 747 Model via Adaptive Modified Two-Stage Kalman Filter
An adaptive modified two-stage linear Kalman filtering algorithm is utilized to identify the loss of control effectiveness and the magnitude of low degree of stuck faults in a closed-loop nonlinear B747 aircraft. Control effectiveness factors and stuck magnitudes are used to quantify faults entering...
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| Main Authors: | , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2014-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2014/472395 |
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| _version_ | 1832553430010298368 |
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| author | Fikret Caliskan Youmin Zhang N. Eva Wu Jong-Yeob Shin |
| author_facet | Fikret Caliskan Youmin Zhang N. Eva Wu Jong-Yeob Shin |
| author_sort | Fikret Caliskan |
| collection | DOAJ |
| description | An adaptive modified two-stage linear Kalman filtering algorithm is utilized to identify the loss of control effectiveness and the magnitude of low degree of stuck faults in a closed-loop nonlinear B747 aircraft. Control effectiveness factors and stuck magnitudes are used to quantify faults entering control systems through actuators. Pseudorandom excitation inputs are used to help distinguish partial loss and stuck faults. The partial loss and stuck faults in the stabilizer are isolated and identified successfully. |
| format | Article |
| id | doaj-art-da959bd7635848c398ea91a75a6828e6 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2014-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-da959bd7635848c398ea91a75a6828e62025-02-03T05:54:07ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742014-01-01201410.1155/2014/472395472395Actuator Fault Diagnosis in a Boeing 747 Model via Adaptive Modified Two-Stage Kalman FilterFikret Caliskan0Youmin Zhang1N. Eva Wu2Jong-Yeob Shin3Department of Control Engineering, Istanbul Technical University, Maslak, 34469 Istanbul, TurkeyDepartment of Mechanical & Industrial Engineering, Concordia University, 1455 de Maisonneuve Boulevard W., Montreal, QC, H3G 1M8, CanadaDepartment of Electrical and Computer Engineering, Binghamton University (SUNY), Binghamton, NY 13902-6000, USAGulfstream Aerospace Corporation, Savannah, GA 31402-2206, USAAn adaptive modified two-stage linear Kalman filtering algorithm is utilized to identify the loss of control effectiveness and the magnitude of low degree of stuck faults in a closed-loop nonlinear B747 aircraft. Control effectiveness factors and stuck magnitudes are used to quantify faults entering control systems through actuators. Pseudorandom excitation inputs are used to help distinguish partial loss and stuck faults. The partial loss and stuck faults in the stabilizer are isolated and identified successfully.http://dx.doi.org/10.1155/2014/472395 |
| spellingShingle | Fikret Caliskan Youmin Zhang N. Eva Wu Jong-Yeob Shin Actuator Fault Diagnosis in a Boeing 747 Model via Adaptive Modified Two-Stage Kalman Filter International Journal of Aerospace Engineering |
| title | Actuator Fault Diagnosis in a Boeing 747 Model via Adaptive Modified Two-Stage Kalman Filter |
| title_full | Actuator Fault Diagnosis in a Boeing 747 Model via Adaptive Modified Two-Stage Kalman Filter |
| title_fullStr | Actuator Fault Diagnosis in a Boeing 747 Model via Adaptive Modified Two-Stage Kalman Filter |
| title_full_unstemmed | Actuator Fault Diagnosis in a Boeing 747 Model via Adaptive Modified Two-Stage Kalman Filter |
| title_short | Actuator Fault Diagnosis in a Boeing 747 Model via Adaptive Modified Two-Stage Kalman Filter |
| title_sort | actuator fault diagnosis in a boeing 747 model via adaptive modified two stage kalman filter |
| url | http://dx.doi.org/10.1155/2014/472395 |
| work_keys_str_mv | AT fikretcaliskan actuatorfaultdiagnosisinaboeing747modelviaadaptivemodifiedtwostagekalmanfilter AT youminzhang actuatorfaultdiagnosisinaboeing747modelviaadaptivemodifiedtwostagekalmanfilter AT nevawu actuatorfaultdiagnosisinaboeing747modelviaadaptivemodifiedtwostagekalmanfilter AT jongyeobshin actuatorfaultdiagnosisinaboeing747modelviaadaptivemodifiedtwostagekalmanfilter |