Abstract
This paper presents the design of a Multi-Input Multi-Output (MIMO) PID controller for a twin-rotor MIMO system. A multivariable control system consisting of two loops is designed for a non-linear system with two inputs and two outputs. The designed controllers have been tested on a simulated model with different possibilities and real-time results were taken. The designed PID controller efficiently controls the loops of the system and does not suffer from any process interactions. The results indicate that the performance of the PID controllers is excellent and both the transient and the steady-state enactment are adequate. The yaw and pitch rotor’s real-time responses are almost the same as the desired ones.
Highlights
Helicopters have been widely used for fast or immediate transports like medical emergencies, personal use, crime prevention, traffic conditioning, fire detection, etc. [1]
This paper presents the design of a Multi-Input MultiOutput (MIMO) PID controller for a twin rotor MIMO system
The designed behavior of the yaw angle for the Twin Rotor MIMO System (TRMS) versus time is presented with different line patterns for desired and actual position
Summary
Muhammad Asad Substation Automation Engineer NG CSD-C, Saudi Electricity Company. Abstract—This paper presents the design of a Multi-Input MultiOutput (MIMO) PID controller for a twin-rotor MIMO system. A multivariable control system consisting of two loops is designed for a non-linear system with two inputs and two outputs. The designed controllers have been tested on a simulated model with different possibilities and real-time results were taken. The designed PID controller efficiently controls the loops of the system and does not suffer from any process interactions. The results indicate that the performance of the PID controllers is excellent and both the transient and the steady-state enactment are adequate. The yaw and pitch rotor’s real-time responses are almost the same as the desired ones
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