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Output-Feedback Stabilization of the PVTOL Aircraft System Based on an Exact Differentiator

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Abstract

An output-feedback control strategy for the regulation of a planar vertical take-off and landing aircraft is presented here. The strategy consists of two controllers that work simultaneously. The first controller stabilizes the vertical variable, and is based on a simple feedback-linearization procedure, in combination with a nonlinear controller (which behaves as a terminal slide mode). The other controller stabilizes the horizontal and angular variables to the desired rest position, and was designed using an energy-control method. The velocities were exactly estimated with a second-order sliding-mode observer. Because this observer computes the velocities in finite time, the control strategy can be designed independently. The effectiveness of the closed-loop system was tested through numerical simulations and compared with other control strategies.

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Acknowledgments

This research was supported by the Secretaría de Investigación y Posgrado of the Instituto Politecnico Nacional (SIP-IPN) under Research Grants 20171586 and 20171948.

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Authors and Affiliations

  1. CIC-Instituto Politécnico Nacional, Av. Juan de Dios Bátiz s/n, U.P.A.L.M, Col. San Pedro Zacatenco, A.P. 75476, México, D.F. 07738, Mexico

    Carlos Aguilar-Ibañez & Julio Mendoza-Mendoza

  2. ESCOM-Instituto Politécnico Nacional, Av. Juan de Dios Bátiz s/n, Mexico, D.F. 07738, Ciudad de México, México

    Miguel S. Suarez-Castanon

  3. ESIME AZC-Instituto Politécnico Nacional, Av. de Las Granjas 682, 02250, Ciudad de México, México

    Jose de Jesus Rubio

  4. Control Automático - CINVESTAV del IPN, Av. Instituto Politécnico Nacional 2508, 07360, Ciudad de México, México

    Juan Carlos Martínez-García

Authors
  1. Carlos Aguilar-Ibañez
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  2. Miguel S. Suarez-Castanon
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  3. Julio Mendoza-Mendoza
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  4. Jose de Jesus Rubio
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  5. Juan Carlos Martínez-García
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Corresponding author

Correspondence to Carlos Aguilar-Ibañez.

Additional information

This research was suported by Secretarí a de Investigación y Posgrado del Instituto Politécnico Nacional, under research grants 20160268 and 20161637.

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Aguilar-Ibañez, C., Suarez-Castanon, M.S., Mendoza-Mendoza, J. et al. Output-Feedback Stabilization of the PVTOL Aircraft System Based on an Exact Differentiator. J Intell Robot Syst 90, 443–454 (2018). https://doi.org/10.1007/s10846-017-0660-0

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  • DOI: https://doi.org/10.1007/s10846-017-0660-0

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