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book chapter · Cambridge University Press eBooks · 2023

Feedback Control

Rafael Palacios, Carlos E. S. Cesnik

Cited by 0Abstract and details only

Abstract

The basic control architecture for flexible aircraft is introduced. Both linear and nonlinear optimal control methods are considered in a sequential manner. First, the theory of linear-quadratic regulators is described, and applied to simple aeroelastic problems. A linear estimator is then introduced thus resulting in linear quadratic Gaussian (LQG) control, which is also exemplified. Finally, the approach is expanded to nonlinear problems with a short introduction to model predictive control theory and its application to flexible aircraft. Some recent numerical results are included to illustrate the potential of this technique.

Cite this paper

APA 7

Palacios, R., & Cesnik, C. E. S. (2023). Feedback Control. Cambridge University Press eBooks, 406–447. https://doi.org/10.1017/9781108354868.011

MLA 9

Palacios, Rafael, and Carlos E. S. Cesnik. “Feedback Control.” Cambridge University Press eBooks, 2023, pp. 406–47, https://doi.org/10.1017/9781108354868.011.

Chicago

Palacios, Rafael, and Carlos E. S. Cesnik. 2023. “Feedback Control.” Cambridge University Press eBooks: 406–47. https://doi.org/10.1017/9781108354868.011.

Harvard

Palacios, R. and Cesnik, C.E.S. (2023) ‘Feedback Control’, Cambridge University Press eBooks, pp. 406–447. Available at: https://doi.org/10.1017/9781108354868.011.

BibTeX
@incollection{palacios2023feedback,
  title = {{Feedback Control}},
  author = {Palacios, Rafael and Cesnik, Carlos E. S.},
  booktitle = {Cambridge University Press eBooks},
  pages = {406--447},
  year = {2023},
  doi = {10.1017/9781108354868.011}
}

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