Fin failure tolerant control of agile air vehicle using feedback linearization
The probability of actuator lock, control surface damage, and thermal insulation failure on supersonic aircraft due to high speed and temperature is significant. Additionally, foldable fins are often used in missiles to increase the number of missiles that can be loaded onto a launcher and facilitat...
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| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
SAGE Publishing
2025-01-01
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| Series: | Measurement + Control |
| Online Access: | https://doi.org/10.1177/00202940241229303 |
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