Abstract

Unmanned Aerial Vehicle (UAV) commonly used for various missions, such as aerial surveillance, remote sensing, transport or search and rescue. UAV with four propeller, known as Quadcopter, is one of UAV known for high flexibility and mobility in narrow area. This paper will study response of a quadcopter with internal disturbance for rolling, pitching, yawing and altitude. The attitude data of quadcopter are numerically simulated. After integrating PID controllers into the systems, quadcopter settling time of roll and pitch systems are 1.419 seconds, yaw system is 2.327 seconds and altitude hold system is 6.339 seconds.

Original languageEnglish
Title of host publicationICAMIMIA 2015 - International Conference on Advanced Mechatronics, Intelligent Manufacture, and Industrial Automation, Proceeding - In conjunction with Industrial Mechatronics and Automation Exhibition, IMAE
PublisherInstitute of Electrical and Electronics Engineers Inc.
Pages34-37
Number of pages4
ISBN (Electronic)9781467373463
DOIs
Publication statusPublished - 8 Jul 2016
Event2015 International Conference on Advanced Mechatronics, Intelligent Manufacture, and Industrial Automation, ICAMIMIA 2015 - Surabaya, Indonesia
Duration: 15 Oct 201516 Oct 2015

Publication series

NameICAMIMIA 2015 - International Conference on Advanced Mechatronics, Intelligent Manufacture, and Industrial Automation, Proceeding - In conjunction with Industrial Mechatronics and Automation Exhibition, IMAE

Conference

Conference2015 International Conference on Advanced Mechatronics, Intelligent Manufacture, and Industrial Automation, ICAMIMIA 2015
Country/TerritoryIndonesia
CitySurabaya
Period15/10/1516/10/15

Keywords

  • UAV
  • quadcopter
  • simulation
  • stability

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