Hexacopter Construction, Autopilot Installation And Flight Testing

Zaw Ko Ko Latt; Kan Nyunt; Moe Kyaw Naing

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Hexacopter Construction, Autopilot Installation And Flight Testing

Zaw Ko Ko Latt Kan Nyunt Moe Kyaw Naing

Subject area: Science,Engineering and Technology · Area of research: Aerospace Engineering

Abstract

Flight data are required to design a control system of a hexacopter. In this paper a hexacopter has been constructed, flight test has been done by using autopilot. Roll, pitch and yaw data are collected and has been plotted.

Keywords

Hexacopter, Pixhawk Autopilot, Flight Test data

References

[1] T. Magnusson, “Attitude Control of a Hexarotor”, Master Thesis, Linkoping universitet, Sweden, 2014.

[2] D. A. Tesch, D. Eckhard, W. C. Guarienti, “Automatic Tuning of Hexacopter Attitude ControlSystems with Experimental Validation”, 21st International Conference on System Theory, Control and Computing (ICSTCC), 2017.

[3] M. A. Cunningham, “Open -Loop System Identification of a Small Multirotor Vehicle with an Active Feedback Control System”. AIAA AVIATION Forum, 2018 Atmospheric Flight Mechanics Conference, pp.2018–3475, Georgia, 2018.

[4] N. Ohlsson, M. Stahl, “A Model-Based Approach to Computer Vision and Automatic Control using Matlab Simulink for an Autonomous Indoor Multirotor UAV”, Master of Science Thesis, CHALMERS UNIVERSITY OF TECHNOLOGY, Goteborg, Sweden 2013.

[5] D.K. Le, T.K. Nam, “A study on the modeling of a hexacopter”, Journal of the Korean Society of Marine Engineering, Vol. 39, No. 10 pp. 1023– 1030, 2015.

[6] A. Julkananusart and I. Nilkhamhang, “Quadrotor Tuning for Attitude Control based on Double- Loop PID Controller using Fictitious Reference Iterative Tuning (FRIT)”, IEC ON2015, pp.004865–004870, 2015.

[7] D. A. Tesch , D. Eckhard , W. C. Guarienti , “Pitch and Roll control of a Quadcopter using Cascade Iterative Feedback Tuning”, 4th IFAC Symposium on Telematics Applications,2016.

[8] WEBOLOGRAPHY: www.pixhawk.org, www.ardupilot.org, www.tarotrc.com, www.helipal.com

How to cite this paper

Zaw Ko Ko Latt, Kan Nyunt, Moe Kyaw Naing "Hexacopter Construction, Autopilot Installation And Flight Testing" Iconic Research And Engineering Journals Volume 3 Issue 1 2019 Page 332-335

Zaw Ko Ko Latt, Kan Nyunt, Moe Kyaw Naing "Hexacopter Construction, Autopilot Installation And Flight Testing" Iconic Research And Engineering Journals, vol. 3, no. 1, Jul. 2019

Zaw Ko Ko Latt, Kan Nyunt, Moe Kyaw Naing (2019). Hexacopter Construction, Autopilot Installation And Flight Testing. Iconic Research And Engineering Journals, 3(1).

Zaw Ko Ko Latt, Kan Nyunt, Moe Kyaw Naing "Hexacopter Construction, Autopilot Installation And Flight Testing" Iconic Research And Engineering Journals, vol. 3, no. 1, Jul. 2019.

@article{1701421,
      author = {Zaw Ko Ko Latt, Kan Nyunt, Moe Kyaw Naing},
      title = {Hexacopter Construction, Autopilot Installation And Flight Testing},
      journal = {Iconic Research And Engineering Journals},
      year = {2019},
      volume = {3},
      number = {1},
      pages = {332-335},
      issn = {2456-8880},
      url = {https://www.irejournals.com/formatedpaper/1701421.pdf},
      abstract = {Flight data are required to design a control system of a hexacopter. In this paper a hexacopter has been constructed, flight test has been done by using autopilot. Roll, pitch and yaw data are collected and has been plotted.},
      keywords = {Hexacopter, Pixhawk Autopilot, Flight Test data},
      month = {July},
  }