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A Simple Approach to Regulate a PVTOL System Using Matching Conditions
In this work, based on shaping an energy function, it is introduced an output-feedback regulation control law for a Planar Vertical Takeoff and Landing (PVTOL) aircraft. To this end, a version of the matching control energy method is used to construct the Lyapunov candidate function and the stabiliz...
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Published in: | Journal of intelligent & robotic systems 2020-05, Vol.98 (2), p.511-524 |
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container_title | Journal of intelligent & robotic systems |
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creator | Aguilar-Ibanez, Carlos Suarez-Castanon, Miguel S. Meda-Campaña, Jesus Gutierrez-Frias, Octavio Merlo-Zapata, Carlos Martinez-Castro, Jesus A. |
description | In this work, based on shaping an energy function, it is introduced an output-feedback regulation control law for a Planar Vertical Takeoff and Landing (PVTOL) aircraft. To this end, a version of the matching control energy method is used to construct the Lyapunov candidate function and the stabilizer controller to regulate the PVTOL aircraft. The non-measurable system velocities are recovered using a suitable exact differentiator observer, achieved through super-twisting based observer. The theorem of LaSalle, together with some tools from the cascade system theory, was used to carry out the closed-loop stability analysis. Using a suitable finite time-varying identificator, the obtained controllers were improved to compensate bounded, smooth, and matching perturbations. Numerical simulations were included to test the effectiveness of the obtained controller. |
doi_str_mv | 10.1007/s10846-019-01087-x |
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To this end, a version of the matching control energy method is used to construct the Lyapunov candidate function and the stabilizer controller to regulate the PVTOL aircraft. The non-measurable system velocities are recovered using a suitable exact differentiator observer, achieved through super-twisting based observer. The theorem of LaSalle, together with some tools from the cascade system theory, was used to carry out the closed-loop stability analysis. Using a suitable finite time-varying identificator, the obtained controllers were improved to compensate bounded, smooth, and matching perturbations. 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subjects | Aircraft Analysis Artificial Intelligence Computer simulation Control Control stability Control theory Controllers Electrical Engineering Engineering Matching Mechanical Engineering Mechatronics Numerical analysis Output feedback Robotics Stability analysis System theory Systems theory Twisting Vertical landing Vertical takeoff |
title | A Simple Approach to Regulate a PVTOL System Using Matching Conditions |
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