Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode
A new method of integrated guidance and control for homing missiles with actuator fault against manoeuvring targets is proposed. Model of the integrated guidance and control system in the pitch plane with actuator fault and some uncertainty is developed. A control law using combination of adaptive b...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Wiley
2015-01-01
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| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2015/253478 |
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| _version_ | 1832548683562876928 |
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| author | Mohsen Fathi Jegarkandi Asghar Ashrafifar Reza Mohsenipour |
| author_facet | Mohsen Fathi Jegarkandi Asghar Ashrafifar Reza Mohsenipour |
| author_sort | Mohsen Fathi Jegarkandi |
| collection | DOAJ |
| description | A new method of integrated guidance and control for homing missiles with actuator fault against manoeuvring targets is proposed. Model of the integrated guidance and control system in the pitch plane with actuator fault and some uncertainty is developed. A control law using combination of adaptive backstepping and sliding mode approaches is designed to achieve interception in the presence of bounded uncertainties and actuator fault. Simulation results show that new approach has better performance than adaptive backstepping and has good performance in the presence of actuator fault. |
| format | Article |
| id | doaj-art-80dae669be184eceb81904e2ca28067c |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2015-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-80dae669be184eceb81904e2ca28067c2025-02-03T06:13:25ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742015-01-01201510.1155/2015/253478253478Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding ModeMohsen Fathi Jegarkandi0Asghar Ashrafifar1Reza Mohsenipour2Department of Aerospace Engineering, Sharif University of Technology, P.O. Box 11365-11155, Tehran, IranDepartment of Aerospace Engineering, Sharif University of Technology, P.O. Box 11365-11155, Tehran, IranDepartment of Aerospace Engineering, Sharif University of Technology, P.O. Box 11365-11155, Tehran, IranA new method of integrated guidance and control for homing missiles with actuator fault against manoeuvring targets is proposed. Model of the integrated guidance and control system in the pitch plane with actuator fault and some uncertainty is developed. A control law using combination of adaptive backstepping and sliding mode approaches is designed to achieve interception in the presence of bounded uncertainties and actuator fault. Simulation results show that new approach has better performance than adaptive backstepping and has good performance in the presence of actuator fault.http://dx.doi.org/10.1155/2015/253478 |
| spellingShingle | Mohsen Fathi Jegarkandi Asghar Ashrafifar Reza Mohsenipour Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode International Journal of Aerospace Engineering |
| title | Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode |
| title_full | Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode |
| title_fullStr | Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode |
| title_full_unstemmed | Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode |
| title_short | Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode |
| title_sort | adaptive integrated guidance and fault tolerant control using backstepping and sliding mode |
| url | http://dx.doi.org/10.1155/2015/253478 |
| work_keys_str_mv | AT mohsenfathijegarkandi adaptiveintegratedguidanceandfaulttolerantcontrolusingbacksteppingandslidingmode AT asgharashrafifar adaptiveintegratedguidanceandfaulttolerantcontrolusingbacksteppingandslidingmode AT rezamohsenipour adaptiveintegratedguidanceandfaulttolerantcontrolusingbacksteppingandslidingmode |