Sensitivity analysis of intelligent active force control applied to a quadrotor system

This paper introduces a hybrid controller to be employed for stabilizing a quadrotor, as an example of rotor unmanned aerial vehicle (UAV) systems, and efficiently repelling the applied perturbations during trajectory tracking in a complex environment via a simulation study. In this study, Newton-Eu...

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Main Authors: Abdelmaksoud, Sherif I., Mailah, Musa, Abdallah, Ayman M.
Format: Conference or Workshop Item
Published: 2022
Subjects:
Online Access:http://eprints.utm.my/id/eprint/101084/
http://dx.doi.org/10.1007/978-3-030-85990-9_14
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spelling my.utm.1010842023-05-27T07:43:37Z http://eprints.utm.my/id/eprint/101084/ Sensitivity analysis of intelligent active force control applied to a quadrotor system Abdelmaksoud, Sherif I. Mailah, Musa Abdallah, Ayman M. Q Science (General) QA75 Electronic computers. Computer science This paper introduces a hybrid controller to be employed for stabilizing a quadrotor, as an example of rotor unmanned aerial vehicle (UAV) systems, and efficiently repelling the applied perturbations during trajectory tracking in a complex environment via a simulation study. In this study, Newton-Euler’s method was used to find the equations of motion for the dynamic model of the quadrotor system taking into account the effects of aerodynamic, gyroscopic, perturbation, and friction. The proposed control structure was comprised of a proportional-integral-derivative (PID) control scheme and an innovative control technique known as active force control (AFC). The AFC was tuned intelligently using artificial intelligence (AI)-based approach, namely, iterative learning algorithm (ILA), to be defined as intelligent active force control (IAFC), and the proposed strategy was identified as (PID-ILAFC) scheme. To evaluate the feasibility of the proposed control scheme, a sinusoidal wave disturbance was introduced as an example of external perturbation. In this study, a sensitivity analysis was also performed considering the variance of the estimated inertia value, model uncertainty, and the AFC output signal percentage to achieve the best possible performance. The outcomes show the efficacy of the IAFC-based strategy in expelling off the applied perturbations and uncertainties in comparison with the PID controller. The results also indicate the importance of the accurate selection of the estimated inertia value to enhance the effectiveness of the AFC approach and the significance of using the full output of the AFC signal to obtain the best performance. 2022 Conference or Workshop Item PeerReviewed Abdelmaksoud, Sherif I. and Mailah, Musa and Abdallah, Ayman M. (2022) Sensitivity analysis of intelligent active force control applied to a quadrotor system. In: International Conference on Emerging Technologies and Intelligent Systems, ICETIS 2021, 25 June 2021 - 26 June 2021, Al Buraimi, Oman. http://dx.doi.org/10.1007/978-3-030-85990-9_14
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
topic Q Science (General)
QA75 Electronic computers. Computer science
spellingShingle Q Science (General)
QA75 Electronic computers. Computer science
Abdelmaksoud, Sherif I.
Mailah, Musa
Abdallah, Ayman M.
Sensitivity analysis of intelligent active force control applied to a quadrotor system
description This paper introduces a hybrid controller to be employed for stabilizing a quadrotor, as an example of rotor unmanned aerial vehicle (UAV) systems, and efficiently repelling the applied perturbations during trajectory tracking in a complex environment via a simulation study. In this study, Newton-Euler’s method was used to find the equations of motion for the dynamic model of the quadrotor system taking into account the effects of aerodynamic, gyroscopic, perturbation, and friction. The proposed control structure was comprised of a proportional-integral-derivative (PID) control scheme and an innovative control technique known as active force control (AFC). The AFC was tuned intelligently using artificial intelligence (AI)-based approach, namely, iterative learning algorithm (ILA), to be defined as intelligent active force control (IAFC), and the proposed strategy was identified as (PID-ILAFC) scheme. To evaluate the feasibility of the proposed control scheme, a sinusoidal wave disturbance was introduced as an example of external perturbation. In this study, a sensitivity analysis was also performed considering the variance of the estimated inertia value, model uncertainty, and the AFC output signal percentage to achieve the best possible performance. The outcomes show the efficacy of the IAFC-based strategy in expelling off the applied perturbations and uncertainties in comparison with the PID controller. The results also indicate the importance of the accurate selection of the estimated inertia value to enhance the effectiveness of the AFC approach and the significance of using the full output of the AFC signal to obtain the best performance.
format Conference or Workshop Item
author Abdelmaksoud, Sherif I.
Mailah, Musa
Abdallah, Ayman M.
author_facet Abdelmaksoud, Sherif I.
Mailah, Musa
Abdallah, Ayman M.
author_sort Abdelmaksoud, Sherif I.
title Sensitivity analysis of intelligent active force control applied to a quadrotor system
title_short Sensitivity analysis of intelligent active force control applied to a quadrotor system
title_full Sensitivity analysis of intelligent active force control applied to a quadrotor system
title_fullStr Sensitivity analysis of intelligent active force control applied to a quadrotor system
title_full_unstemmed Sensitivity analysis of intelligent active force control applied to a quadrotor system
title_sort sensitivity analysis of intelligent active force control applied to a quadrotor system
publishDate 2022
url http://eprints.utm.my/id/eprint/101084/
http://dx.doi.org/10.1007/978-3-030-85990-9_14
_version_ 1768006606562263040
score 13.160551