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Robust control of a nonlinear non-minimum phase supersonic flight vehicle based on stable system center

  • Published:2013-03 Issue:1 Volume:25 Page:283-291
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Bahrami Mohsen,Ebrahimi Behrouz,Asadi Mehdi

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference13 articles.

1. Dynamic sliding mode autopilot for nonlinear non-minimum phase flight vehicle;Bahrami;Transactions of the Japan Society for Aeronautical and Space Sciences,2009

2. Output regulation for nonlinear systems: An overview;Byrnes;International Journal of Robust and Nonlinear Control,2000

3. Nonlinear inversion-based output tracking;Devasia;IEEE Transactions on Automatic Control,1996

4. Tracking nonlinear non-minimum phase system using sliding control;Gopalswmy;International Journal of Control,1993

5. Nonlinear Control Systems;Isidori,1995

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1. Robust gain-scheduled missile autopilot design based on multifrequency extended state observers;Chinese Journal of Aeronautics;2023-12

2. Approximate stable system centre approach to output tracking of non-minimum phase nonlinear systems;Journal of the Franklin Institute;2017-05

3. A gradient descent control for output tracking of a class of non-minimum phase nonlinear systems;Journal of Applied Research and Technology;2016-12

4. Model Predictive Controllers for Nonminimum-phase Quadruple-tank Process;Advances in Intelligent Systems and Computing;2014-11-02

5. Backstepping attitude control for hypersonic gliding vehicle based on a robust dynamic inversion approach;Proceedings of the Institution of Mechanical Engineers, Part I: Journal of Systems and Control Engineering;2014-06-08
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