Fin failure tolerant control of agile air vehicle using feedback linearization
Asghar Ashrafifar,
Mohsen Fathi Jegarkandi
Abstract: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 facilitate transportation, but this design presents the potential for malfunction and failure to open during flight. This study focuses on scenarios where control surfaces do not open or are partially damaged, leading to asy… Show more
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