A Practical Guideline for Designing and Tuning Adaptive Backstepping Controllers for a Class of Second-Order Systems based on PID Similarity
| dc.contributor.author | Kourani, Ahmad | |
| dc.contributor.author | Daher, Naseem A. | |
| dc.contributor.department | Department of Mechanical Engineering | |
| dc.contributor.department | Department of Electrical and Computer Engineering | |
| dc.contributor.faculty | Maroun Semaan Faculty of Engineering and Architecture (MSFEA) | |
| dc.contributor.institution | American University of Beirut | |
| dc.date.accessioned | 2025-01-24T11:33:22Z | |
| dc.date.available | 2025-01-24T11:33:22Z | |
| dc.date.issued | 2022 | |
| dc.description.abstract | Abstract: This work proposes a practical guideline for designing and tuning adaptive backstepping control systems by leveraging the similarity with PID control laws for a class of second-order nonlinear systems. A complete set of mathematical formulations, visual aids, and a well-structured algorithm are provided to exploit the benefits of the established link. This aims at facilitating the adoption of advanced nonlinear control laws in more real-life and industrial applications while benefiting from the legacy of PID tuning rules. Furthermore, the proposed guideline allows for upgrading primitive PID controllers to more advanced nonlinear control system. The adaptive backstepping control law is formulated as a two degrees-of-freedom control law that combines the sum of a feedback PID control component and a feedforward model compensation component. The relationship between backstepping and PID gains is provided in the form of a third-order polynomial, and a simplified second-order one, with practical design algorithm and tuning guidelines. The proposed control law and tuning methodology are validated on a quadrotor unmanned aerial vehicle (UAV) system in both simulation and experimentally. © 2022, The Author(s), under exclusive licence to Springer-Verlag GmbH Germany, part of Springer Nature. | |
| dc.identifier.doi | https://doi.org/10.1007/s40435-022-00922-8 | |
| dc.identifier.eid | 2-s2.0-85126018571 | |
| dc.identifier.uri | http://hdl.handle.net/10938/27973 | |
| dc.language.iso | en | |
| dc.publisher | Springer Science and Business Media Deutschland GmbH | |
| dc.relation.ispartof | International Journal of Dynamics and Control | |
| dc.source | Scopus | |
| dc.subject | Adaptive backstepping control | |
| dc.subject | Lyapunov stability | |
| dc.subject | Pid tuning | |
| dc.subject | Quadrotor uav | |
| dc.subject | Adaptive control systems | |
| dc.subject | Aircraft control | |
| dc.subject | Antennas | |
| dc.subject | Backstepping | |
| dc.subject | Control theory | |
| dc.subject | Controllers | |
| dc.subject | Degrees of freedom (mechanics) | |
| dc.subject | Unmanned aerial vehicles (uav) | |
| dc.subject | Adaptive backstepping | |
| dc.subject | Backstepping controller | |
| dc.subject | Control laws | |
| dc.subject | Practical guidelines | |
| dc.subject | Quadrotor unmanned aerial vehicles | |
| dc.subject | Second-order nonlinear systems | |
| dc.subject | Second-order systemss | |
| dc.subject | Three term control systems | |
| dc.title | A Practical Guideline for Designing and Tuning Adaptive Backstepping Controllers for a Class of Second-Order Systems based on PID Similarity | |
| dc.type | Article |
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