Method of generating an integrated fuzzy-based guidance law for aerodynamic missiles

This invention describes a computer-based method for creating a smart guidance system for missiles. It uses three separate 'fuzzy logic' controllers, each designed to take over at different stages of the missile's flight, like launch, mid-course, and terminal approach. These controllers are developed by a computer program that uses advanced optimization techniques to find the best balance between hitting the target accurately, using less energy, and reaching the target quickly.