Title :
Integration of a fuzzy guidance-control system for a command interceptor against hypersonic target
Author :
Elhalwagy, Y.Z. ; Tarbouchi, M.
Author_Institution :
Dept. of Electr. & Comput. Eng., R. Mil. Coll. of Canada, Kingston, Ont., Canada
Abstract :
Extensive research efforts have been made to design or improve flight guidance and control systems. With the phenomenal growth in soft computing techniques, there is a growing interest to apply these techniques to missile flight guidance and control systems. This paper investigates the application of fuzzy logic for the development of fuzzy guidance laws for command-to-line-of-sight skid-to-turn (CLOS-STT) missile. The fuzzy logic guidance scheme based on the well known three-point guidance law is discussed. Preliminary studies have shown the advantages of using anti-air tactical missiles against hypersonic ballistic targets. A complete six-degrees-of-freedom (6-DOF)-flight model for an anti-air command guidance system is developed. Simulation results for this three-dimensional missile-target interception process are given to show the effectiveness of the proposed fuzzy guidance scheme
Keywords :
fuzzy control; military computing; missile guidance; neural nets; anti-air command guidance system; anti-air tactical missiles; command interceptor; command-to-line-of-sight skid-to-turn missile; fuzzy guidance-control system; hypersonic ballistic targets; hypersonic target; missile flight control systems; missile flight guidance systems; neural networks; six-degrees-of-freedom-flight model; soft computing; three dimensional missile-target interception process; three-point guidance law; Aerodynamics; Computer vision; Control systems; Educational institutions; Fuzzy logic; Fuzzy systems; Intelligent control; Military aircraft; Military computing; Missiles;
Conference_Titel :
Industrial Electronics Society, 2001. IECON '01. The 27th Annual Conference of the IEEE
Conference_Location :
Denver, CO
Print_ISBN :
0-7803-7108-9
DOI :
10.1109/IECON.2001.975607
