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The Scientific World Journal
Volume 2014 (2014), Article ID 280180, 13 pages
Research Article

A Simple Attitude Control of Quadrotor Helicopter Based on Ziegler-Nichols Rules for Tuning PD Parameters

ZeFang He1,2 and Long Zhao1,2

1Science and Technology on Aircraft Control Laboratory, Beihang University, Beijing 100191, China
2Digital Navigation Center, Beihang University, Beijing 100191, China

Received 25 August 2014; Accepted 10 October 2014; Published 29 December 2014

Academic Editor: Wenwu Yu

Copyright © 2014 ZeFang He and Long Zhao. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Citations to this Article [3 citations]

The following is the list of published articles that have cited the current article.

  • ZeFang He, and Long Zhao, “Quadrotor Trajectory Tracking Based on Quasi-LPV System and Internal Model Control,” Mathematical Problems in Engineering, vol. 2015, pp. 1–13, 2015. View at Publisher · View at Google Scholar
  • Oyas Wahyunggoro, Adha Imam Cahyadi, and Iswanto, “Hover position of quadrotor based on PD-like fuzzy linear programming,” International Journal of Electrical and Computer Engineering, vol. 6, no. 5, pp. 2251–2261, 2016. View at Publisher · View at Google Scholar
  • Tiberiu Vesselenyi, Simona Dzitac, Endrowednes Kuantama, and Radu Tarca, “PID and Fuzzy-PID control model for quadcopter attitude with disturbance parameter,” International Journal of Computers, Communications and Control, vol. 12, no. 4, pp. 519–532, 2017. View at Publisher · View at Google Scholar