Online citations, reference lists, and bibliographies.
← Back to Search

Fuzzy Knowledge Based Guidance In The Homing Missiles

Mustafa Resa Becan, A. Kuzucu
Published 2003 · Computer Science

Save to my Library
Download PDF
Analyze on Scholarcy Visualize in Litmaps
Reduce the time it takes to create your bibliography by a factor of 10 by using the world’s favourite reference manager
Time to take this seriously.
Get Citationsy
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.
This paper references

Semantic Scholar Logo Some data provided by SemanticScholar