Development of Fuzzy Logic Controller to Enhance the Performance of a HILS for a Homing Guided Missile | ||||
International Conference on Aerospace Sciences and Aviation Technology | ||||
Article 62, Volume 12, ASAT Conference, 29-31 May 2007, May 2007, Page 1-12 PDF (696.13 K) | ||||
Document Type: Original Article | ||||
DOI: 10.21608/asat.2007.23982 | ||||
View on SCiNiTO | ||||
Authors | ||||
Elhalwagy Y. Z.1; Abdelhady A. M.2; Fahmy A. E.3 | ||||
1Dr. , Dpt. of Radar And Guidance, Military Technical Collage , Cairo, Egypt. | ||||
2Eng. , Dpt. of Radar And Guidance, Military Technical Collage , Cairo, Egypt. | ||||
3Professor , 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. | ||||
Keywords | ||||
Fuzzy Logic controller; Hardware in the loop | ||||
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