The Design of Optimal PID Control Method for Quadcopter Movement Control

Hanum Arrosida(1*), Mohammad Erik Echsony(2),


(1) State Polytechnic of Madiun
(2) State Polytechnic of Madiun
(*) Corresponding Author

Abstract


Nowadays, quadcopter motion control has become a popular research topic because of its versatile ability as an unmanned aircraft can be used to alleviate human labor and also be able to reach dangerous areas or areas which is unreachable to humans. On the other hand, the Optimal PID control method, which incorporates PID and Linear Quadratic Regulator (LQR) control methods, has also been widely used in industry and research field because it has advantages that are easy to operate, easy design, and a good level of precision. In the PID control method, the main problem to be solved is the accuracy of the gain value Kp, Ki, and Kd because the inappropriateness of those value will result in an imprecise control action. Based on these problems and referring to the previous study, the optimal PID control method was developed by using PID controller structure with tuning gain parameter of PID through Linear Quadratic Regulator (LQR) method. Through the integration of these two control methods, the optimum solutions can be obtained: easier controller design process for quadcopter control when crossing the determined trajectories, steady state error values less than 5% and a stable quadcopter movement with roll and pitch angle stabilization at position 0 radians with minimum energy function.

Keywords


Quadcopter; Optimal PID; Tuning Gain; Minimum energy function;

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References


Milionis, Georgios, “A Frame For Collaborative Quadrotor-Ground Robot Missions”, Thesis, Naval Postgraduate, California, 2011.

Arrosida, Hanum. "Perancangan Metode Kontrol LQR (Linear Quadratic Regulator) Sebagai Solusi Optimal Pengendalian Gerak Quadrotor." Seminar MASTER 2016. Vol. 1. No. 1. 2016.

Kardono,”Perancangan dan Implementasi Sistem Pengaturan Optimal LQR untuk Menjaga Kestabilan Hover Pada Quadcopter”, Tugas Akhir, Institut Teknologi Sepuluh Nopember, Surabaya, 2012.

Desineni Subbaram Naidu, “Optimal Control System”, CRC Press, 2003.

Ogata, Katsuhiko, “Teknik Kontrol Automatik –terjemahan Ir. Edi Laksono” Erlangga, Jakarta 1991.

Gamayanti, Nurlita, ”Karakteristik Sistem Ordo Pertama”, Teknik Sistem Pengaturan, Jurusan Teknik Elektro FTI-ITS, Surabaya, 2010.

Rosyid, Dimaz Ma’ruf. “Perancangan dan Implementasi Kontroler PID independent dan Metode Decoupling pada Gerakan Lateral UAV untuk Tracking Waypoint”, Tugas Akhir, Teknik Sistem Pengaturan, Jurusan Teknik Elektro FTI-ITS, Surabaya, 2012.

W. Beard,Randal. “Quadrotor Dynamics and Control”, Brigham Young University, February 19, 2008.

Tommaso Bresciani, “Modelling, Identification and Control of a Quadrotor Helicopter”. Department of Automatic Control Lund University, October 2008.

Arjin, N. Theeerachai, W. (2007), “Design of Decoupled Controller for TITO System using Characteristic Ratio Assignment”, International Conference on Control Automation and Systems, 957-962.

D. Handoko, M. Mesran, S. D. Nasution, Y. Yuhandri, and H. Nurdiyanto, “Application Of Weight Sum Model (WSM) In Determining Special Allocation Funds Recipients,” IJICS (International J. Informatics Comput. Sci., vol. 1, no. 2, Dec. 2017.

Ogata, K. (2002), Modern Control Engineering, 4th edition, Prentice-Hall, New Jersey M. Young, The Technical Writer’s Handbook. Mill Valley, CA: University Science, 1989.




DOI: https://doi.org/10.29099/ijair.v2i1.32

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