Journal of scientific reports-A (Online), cilt.1, sa.52, ss.174-189, 2023 (Hakemli Dergi)
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 (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 (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
(FOPID), proportional-integral-derivative (PID) and tilt-integral-derivative
(TID) controllers.