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Robust PID Controller Design for a Modern Type Aircraft Including Handling Quality Evaluation

Received: 9 March 2014     Published: 30 March 2014
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Abstract

In this paper we present classical PID controller approach in designing longitudinal Stability Augmentation System and pitch attitude control (SCAS) at nonlinear flight region for a high fidelity F-16 model including aerodynamic uncertainty. In high angle of attack, nonlinear effects of aerodynamic coefficients and atmospheric turbulence are the main challenge in designing and robustness of flight control system. A design scenario that combines deadbeat response and robust control (aerodynamic uncertainties and atmospheric turbulence) is presented. Simulation results show that the designed PI controller exhibits robustness property to system uncertainties.

Published in American Journal of Aerospace Engineering (Volume 1, Issue 1)
DOI 10.11648/j.ajae.20140101.11
Page(s) 1-7
Creative Commons

This is an Open Access article, distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium or format, provided the original work is properly cited.

Copyright

Copyright © The Author(s), 2014. Published by Science Publishing Group

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Keywords

Aircraft Pitch Control, Deadbeat Controller, Robust Controller, Modern Type Aircraft

References
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  • APA Style

    Mohammad Salem, Mohammad Ali Shahi Ashtiani. (2014). Robust PID Controller Design for a Modern Type Aircraft Including Handling Quality Evaluation. American Journal of Aerospace Engineering, 1(1), 1-7. https://doi.org/10.11648/j.ajae.20140101.11

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    ACS Style

    Mohammad Salem; Mohammad Ali Shahi Ashtiani. Robust PID Controller Design for a Modern Type Aircraft Including Handling Quality Evaluation. Am. J. Aerosp. Eng. 2014, 1(1), 1-7. doi: 10.11648/j.ajae.20140101.11

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    AMA Style

    Mohammad Salem, Mohammad Ali Shahi Ashtiani. Robust PID Controller Design for a Modern Type Aircraft Including Handling Quality Evaluation. Am J Aerosp Eng. 2014;1(1):1-7. doi: 10.11648/j.ajae.20140101.11

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  • @article{10.11648/j.ajae.20140101.11,
      author = {Mohammad Salem and Mohammad Ali Shahi Ashtiani},
      title = {Robust PID Controller Design for a Modern Type Aircraft Including Handling Quality Evaluation},
      journal = {American Journal of Aerospace Engineering},
      volume = {1},
      number = {1},
      pages = {1-7},
      doi = {10.11648/j.ajae.20140101.11},
      url = {https://doi.org/10.11648/j.ajae.20140101.11},
      eprint = {https://article.sciencepublishinggroup.com/pdf/10.11648.j.ajae.20140101.11},
      abstract = {In this paper we present classical PID controller approach in designing longitudinal Stability Augmentation System and pitch attitude control (SCAS) at nonlinear flight region for a high fidelity F-16 model including aerodynamic uncertainty. In high angle of attack, nonlinear effects of aerodynamic coefficients and atmospheric turbulence are the main challenge in designing and robustness of flight control system. A design scenario that combines deadbeat response and robust control (aerodynamic uncertainties and atmospheric turbulence) is presented. Simulation results show that the designed PI controller exhibits robustness property to system uncertainties.},
     year = {2014}
    }
    

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    AU  - Mohammad Salem
    AU  - Mohammad Ali Shahi Ashtiani
    Y1  - 2014/03/30
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    T2  - American Journal of Aerospace Engineering
    JF  - American Journal of Aerospace Engineering
    JO  - American Journal of Aerospace Engineering
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    UR  - https://doi.org/10.11648/j.ajae.20140101.11
    AB  - In this paper we present classical PID controller approach in designing longitudinal Stability Augmentation System and pitch attitude control (SCAS) at nonlinear flight region for a high fidelity F-16 model including aerodynamic uncertainty. In high angle of attack, nonlinear effects of aerodynamic coefficients and atmospheric turbulence are the main challenge in designing and robustness of flight control system. A design scenario that combines deadbeat response and robust control (aerodynamic uncertainties and atmospheric turbulence) is presented. Simulation results show that the designed PI controller exhibits robustness property to system uncertainties.
    VL  - 1
    IS  - 1
    ER  - 

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Author Information
  • Department of Aerospace Engineering, Aerospace Research Institute, MAUT, Islamic Republic of Iran

  • Department of Aerospace Engineering, Aerospace Research Institute, MAUT, Islamic Republic of Iran

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