Optimal feedback control of a twin rotor MIMO system

Research output: Contribution to journalArticle

4 Citations (Scopus)

Abstract

In this article, optimal feedback control of the twin rotor multiple input-multiple output (MIMO) system is investigated. The twin rotor MIMO system is a benchmark aero-dynamical laboratory model having strongly nonlinear characteristics and unstable coupling dynamics which make the control of such system for either posture stabilization or trajectory tracking a challenging task. This article first briefs the mathematical model of the twin rotor MIMO system and then illustrates the basic idea and technical formulation for controller design. The paper briefly explains the mixed sensitivity design method for feedback control of the twin rotor multiple input-multiple output system laboratory model. This approach has been considered in order to assure high control performance of the system. The simulation results show that the investigated controller has both static and dynamic performance, therefore the stability and the quick control effect can be obtained simultaneously for the twin rotor MIMO system.

Original languageEnglish
Pages (from-to)46-53
Number of pages8
JournalInternational Journal of Modelling and Simulation
Volume37
Issue number1
DOIs
Publication statusPublished - 02-01-2017

Fingerprint

Optimal Feedback Control
Multiple-input multiple-output (MIMO) Systems
Rotor
Feedback control
Rotors
Controllers
Trajectory Tracking
Dynamic Performance
Controller Design
Feedback Control
Design Method
Stabilization
Unstable
Trajectories
Mathematical Model
Mathematical models
Benchmark
Controller
Formulation
Model

All Science Journal Classification (ASJC) codes

  • Software
  • Modelling and Simulation
  • Mechanics of Materials
  • Hardware and Architecture
  • Electrical and Electronic Engineering

Cite this

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Optimal feedback control of a twin rotor MIMO system. / Choudhary, Santosh Kumar.

In: International Journal of Modelling and Simulation, Vol. 37, No. 1, 02.01.2017, p. 46-53.

Research output: Contribution to journalArticle

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