Abstract
A fuzzy knowledge based tail pursuit guidance scheme is proposed as an alternative to the conventional methods. The purpose of this method is to perform the tracking and interception using a simplified guidance law based on the fuzzy controller. Noise effects in homing missile guidance must be reduced to get an accurate control. In this work, developed fuzzy tail pursuit control algorithm reduces the noise effects. Then, a knowledge based algorithm is derived from the fuzzy control behavior to obtain a simplified guidance law. Simulation results show that the new algorithm led to satisfactory performance for the purpose of this work.
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© 2003 Springer-Verlag Berlin Heidelberg
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Becan, M.R., Kuzucu, A. (2003). Fuzzy Knowledge Based Guidance in the Homing Missiles. In: Palade, V., Howlett, R.J., Jain, L. (eds) Knowledge-Based Intelligent Information and Engineering Systems. KES 2003. Lecture Notes in Computer Science(), vol 2773. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-45224-9_36
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DOI: https://doi.org/10.1007/978-3-540-45224-9_36
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