TY - GEN
T1 - LabView based Conrol System Design for VTOL Aircraft System
AU - Fatima, Kehkashan
AU - Idrisi, Amir Hussain
AU - Mourad, Abdel Hamid Ismail
N1 - Publisher Copyright:
© 2020 IEEE.
PY - 2020/2
Y1 - 2020/2
N2 - Vertical Take Off and Landing (VTOL) aircraft system is a highly complicated, nonlinear, and a multi variable large disturbances system. Hence an efficient control mechanism is a difficult task for such system. The key objective of this study is to design a controller which balances the VTOL system parallel to the ground (horizontal position) in spite of disturbances. Design of Proportional Integral Derivative (PID) Controller is chosen because of its simplicity, clear functionality and easy to apply algorithm. This appears to be intuitive but can be hard in practice if multiple objectives such as high stability and reduced oscillations are to be achieved. The system response is examined for various values of controller gains. Also, setpoint filters are introduced to improve the overall performance of the controller. Finally, the experimental and LabVIEW based simulation results for pitch angle and current response (current flowing through motor) are calculated and compared which demonstrate that a proper filter selection based PID controller is an effective algorithm.
AB - Vertical Take Off and Landing (VTOL) aircraft system is a highly complicated, nonlinear, and a multi variable large disturbances system. Hence an efficient control mechanism is a difficult task for such system. The key objective of this study is to design a controller which balances the VTOL system parallel to the ground (horizontal position) in spite of disturbances. Design of Proportional Integral Derivative (PID) Controller is chosen because of its simplicity, clear functionality and easy to apply algorithm. This appears to be intuitive but can be hard in practice if multiple objectives such as high stability and reduced oscillations are to be achieved. The system response is examined for various values of controller gains. Also, setpoint filters are introduced to improve the overall performance of the controller. Finally, the experimental and LabVIEW based simulation results for pitch angle and current response (current flowing through motor) are calculated and compared which demonstrate that a proper filter selection based PID controller is an effective algorithm.
KW - Controller design
KW - LabVIEW
KW - Low-pass filter
KW - PI controller
KW - PID controller
KW - Vertical take-off and landing (VTOL) aircraft
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U2 - 10.1109/ASET48392.2020.9118372
DO - 10.1109/ASET48392.2020.9118372
M3 - Conference contribution
AN - SCOPUS:85087437969
T3 - 2020 Advances in Science and Engineering Technology International Conferences, ASET 2020
BT - 2020 Advances in Science and Engineering Technology International Conferences, ASET 2020
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2020 Advances in Science and Engineering Technology International Conferences, ASET 2020
Y2 - 4 February 2020 through 9 April 2020
ER -