Control Design of Quadcopter using Linear Quadratic Gaussian (LQG)

Mardlijah, Zahra Nur Alifah

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Citations (Scopus)

Abstract

A quadcopter is an unmanned control aircraft with four rotors and is mounted in a square formation. Quadcopter moves with six degrees of freedom that are divided into two types of movements, there are rotational motion and translational motion. The Linear Quadratic Gaussian control method is used in this research, which combines the Linear Quadratic Regulator with Kalman Filter. LQG control was chosen because it can estimate state variables that are not measured, and it can save costs and time. The variables controlled and analyzed in this study are changes in the angle of rotational motion including roll, pitch, and yaw with a fixed linear position. The quadcopter mathematical model has been linearized and shows stability, controllability, and observability. Simulation results show that the system produces an overshoot less than 0.1 rad with a time stable less than 1 second.

Original languageEnglish
Title of host publicationProceeding of the International Conference on Computer Engineering, Network and Intelligent Multimedia, CENIM 2022
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages192-196
Number of pages5
ISBN (Electronic)9781665476508
DOIs
Publication statusPublished - 2022
Event2022 International Conference on Computer Engineering, Network and Intelligent Multimedia, CENIM 2022 - Surabaya, Indonesia
Duration: 22 Nov 202223 Nov 2022

Publication series

NameProceeding of the International Conference on Computer Engineering, Network and Intelligent Multimedia, CENIM 2022

Conference

Conference2022 International Conference on Computer Engineering, Network and Intelligent Multimedia, CENIM 2022
Country/TerritoryIndonesia
CitySurabaya
Period22/11/2223/11/22

Keywords

  • Kalman Filter
  • Linear Quadratic Gaussian
  • Quadcopter
  • Rotational Motion

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