@inproceedings{3bc133eaf33d4592b53e14bcfede5730,
title = "Quadcopter trajectory tracking and attitude control based on euler angle limitation",
abstract = "The aim of this paper is to build a trajectory tracking system considering the attitude of the quadrotor. Nowadays, quadcopter is often used for taking landscape pictures. The roll pitch Euler angle of the quadcopter greatly affects the resulting pictures so that it needs to be controlled. As a limitation, the roll pitch Euler angle based on inertial reference frame is not allowed to be more than fifteen degrees. Two main factors that affect the Euler angle of quadcopter are velocity and acceleration. Therefore, the velocity and acceleration of the UAV is maintained. A linear regression method is used to determine the velocity and acceleration reference that affect the resulting Euler angle. PID (Proportional, Integral, Derivative) controller is used as the controller method for the tracking control system. Finally, the trajectory tracking and attitude control is evaluated through simulation with ROS and Gazebo.",
keywords = "Attitude control, Euler angle, Gazebo, PID, Quadcopter, ROS, Trajectory tracking",
author = "Billie Pratama and Abdul Muis and Aries Subiantoro and Mohamed Djemai and {Ben Atitallah}, Rabie",
year = "2018",
month = oct,
day = "1",
doi = "10.1109/CEIT.2018.8751819",
language = "English",
series = "2018 6th International Conference on Control Engineering and Information Technology, CEIT 2018",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
editor = "Arisoy, {Dogan Onur} and Engin, {Seref Naci} and Oz, {Muhammed Ali}",
booktitle = "2018 6th International Conference on Control Engineering and Information Technology, CEIT 2018",
address = "United States",
note = "6th International Conference on Control Engineering and Information Technology, CEIT 2018 ; Conference date: 25-10-2018 Through 27-10-2018",
}