TY - GEN
T1 - Control Design of Quadcopter using Output Feedback Control Pole Placement
AU - Mardlijah,
AU - Prihatini, Dita
N1 - Publisher Copyright:
© 2022 IEEE.
PY - 2022
Y1 - 2022
N2 - A Quadcopter is an UAV or unmanned aircraft with four rotors in a square formation that may be operated remotely, necessitating a control system. The Quadcopter mathematical model used is linear and the Quadcopter can move both rotationally and translationally. In this research, system analysis and control design were carried out using the Output Feedback Control Pole Placement method to control the roll angle and pitch angle, to maintain stability by increasing the performance of the Quadcopter system. The Quadcopter dynamic system analysis results are stable, controllable, and observable. The control design is carried out using three feedback gain scenarios (K1K2, and K3) to adjust the eigenvalues so that they are stable. Based on the simulation results of roll and pitch angles, it is concluded that the third scenario (K3) with the fastest stable time, and the first scenario (K1) with the lowest overshoot value.
AB - A Quadcopter is an UAV or unmanned aircraft with four rotors in a square formation that may be operated remotely, necessitating a control system. The Quadcopter mathematical model used is linear and the Quadcopter can move both rotationally and translationally. In this research, system analysis and control design were carried out using the Output Feedback Control Pole Placement method to control the roll angle and pitch angle, to maintain stability by increasing the performance of the Quadcopter system. The Quadcopter dynamic system analysis results are stable, controllable, and observable. The control design is carried out using three feedback gain scenarios (K1K2, and K3) to adjust the eigenvalues so that they are stable. Based on the simulation results of roll and pitch angles, it is concluded that the third scenario (K3) with the fastest stable time, and the first scenario (K1) with the lowest overshoot value.
KW - Output Feedback Control Pole Placement
KW - Quadcopter
KW - UAV
UR - http://www.scopus.com/inward/record.url?scp=85149145098&partnerID=8YFLogxK
U2 - 10.1109/CENIM56801.2022.10037547
DO - 10.1109/CENIM56801.2022.10037547
M3 - Conference contribution
AN - SCOPUS:85149145098
T3 - Proceeding of the International Conference on Computer Engineering, Network and Intelligent Multimedia, CENIM 2022
SP - 197
EP - 202
BT - Proceeding of the International Conference on Computer Engineering, Network and Intelligent Multimedia, CENIM 2022
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2022 International Conference on Computer Engineering, Network and Intelligent Multimedia, CENIM 2022
Y2 - 22 November 2022 through 23 November 2022
ER -