Development of Fuzzy Logic Controller to Enhance the Performance of a HILS for a Homing Guided Missile

Document Type : Original Article

Authors

1 Dr. , Dpt. of Radar And Guidance, Military Technical Collage , Cairo, Egypt.

2 Eng. , Dpt. of Radar And Guidance, Military Technical Collage , Cairo, Egypt.

3 Professor , Dpt. of Radar And Guidance, Military Technical Collage , Cairo, Egypt.

Abstract

This paper investigates the application of fuzzy logic for the development of guidance commands for homing missiles. Fuzzy logic approximation of the well-known proportional navigation guidance law is discussed to enhance the interception of targets performing uncertain maneuvers. Fuzzy logic guidance law development employs triangular membership functions. Simulation results using a HILS system are given.

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