EVALUATION OF CONTROLLER PARAMETERS ON THE TWIN ROTOR MULTIPLE INPUT MULTIPLE OUTPUT SYSTEM USING BUTTERFLY-BASED PARTICLE SWARM OPTIMIZATION

Authors : Ali Can ÇABUKER, Mehmet Nuri ALMALI, İshak PARLAR

Pages : 174-189

Doi:10.59313/jsr-a.1198441

View : 30 | Download : 8

Publication Date : 2023-03-29

Article Type : Research Paper

Abstract :Studies on the control of nonlinear systems with metaheuristic algorithms are increasing day by day. It is one of the nonlinear systems in the Twin rotor multiple input multiple output insert ignore into journalissuearticles values(TRMS); system, which emerged as a prototype of helicopters. This system has two control angles horizontally and vertically. In this study, the yaw and pitch angle control parameters of the TRMS system were found using both traditional and butterfly-based particle swarm optimization insert ignore into journalissuearticles values(BFPSO); method. In experimental studies, reference values of main propeller and tail propeller angles were tried to be reached in TRMS with fractional order proportional-integral-derivative insert ignore into journalissuearticles values(FOPID);, proportional-integral-derivative insert ignore into journalissuearticles values(PID); and tilt-integral-derivative insert ignore into journalissuearticles values(TID); controllers.
Keywords : TRMS, Pitch Angle, Yaw Angle, BFPSO, PID, FOPID, TID

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