AGILE FLIGHT VEHICLE FIN FAILURE TOLERANT CONTROL USING INERTIAL MEASUREMENT UNIT DATA
In this paper, a new model-based fault detection method for an agile supersonic flight vehicle is presented. A nonlinear model, controlled by a classical closed loop controller an...
| Main Authors: | , |
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| Format: | Article |
| Language: | fas |
| Published: |
Sharif University of Technology
2020-05-01
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| Series: | مهندسی مکانیک شریف |
| Subjects: | |
| Online Access: | https://sjme.journals.sharif.edu/article_21645_ab58026202bd5cc40fc08dba97a8b3c5.pdf |