Title of article
Design of aerospace control systems using fractional PID controller
Author/Authors
Aboelela, Magdy A.S. Cairo University - Faculty of Engineering - Electric Power and Machines Department, Egypt , Ahmed, Mohamed F. Egyptian Armed Forces, Egypt , Dorrah, Hassen T. Cairo University - Faculty of Engineering - Electrical Power and Machines Department, Egypt
From page
225
To page
232
Abstract
The goal is to control the trajectory of the flight path of six degree of freedom flying body model using fractional PID. The design of fractional PID controller for the six degree of freedom flying body is described. The parameters of fractional PID controller are optimized by particle swarm optimization (PSO) method. In the optimization process, various objective functions were considered and investigated to reflect both improved dynamics of the missile system and reduced chattering in the control signal of the controller.
Keywords
Six degree of freedom missile model , Particle swarm optimization , Fractional PID control , Matlab , Simulink
Journal title
Journal of Advanced Research
Journal title
Journal of Advanced Research
Record number
2593473
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