The dynamics, prediction, and control of wing rock in high–performance aircraft-Reference-Cited by-同舟云学术

The dynamics, prediction, and control of wing rock in high–performance aircraft

Published:1998-10-15 Issue:1745 Volume:356 Page:2257-2276
ISSN:1364-503X
Container-title:Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences
language:en
Short-container-title:Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences

Author:

Liebst Brad S.¹

Affiliation:

1. Air Force Institute of Technology, Wright-Patterson Air Force Base, OH 45433, USA

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

Link

https://royalsocietypublishing.org/doi/pdf/10.1098/rsta.1998.0273

Reference22 articles.

1. Air Force Flight Test Center 1976 F-15A approach-to-stall/stall/post stall evaluation. AFFTCTR-75-3 (January AD-B045115). Edwards AFB CA: HQ AFFTC.

2. Araujo A. & Singh S. 1997 Variable structure adaptive control of wing rock motion of slender delta wings. In AIAA Atmospheric Flight Mechanics Conf. paper no. 97-3488. Washington DC: American Institute of Aeronautics and Astronautics.

3. Barth T. J. 1987 Determination of high angle-of-attack stability of the F-15B aircraft using bifurcation analysis. MS thesis AFIT/GAE/AA/87D-1. School of Engineering Air Force Institute of Technology (AU) Wright-Patterson AFB OH.

4. Beck J. A. 1989 Bifurcation analysis of a model fighter aircraft with control augmentation. MS thesis AFIT/GAE/ENY/89D-02. School of Engineering Air Force Institute of Technology (AU) Wright-Patterson AFB OH.

5. Bifurcation Analysis of Nonlinear Aircraft Dynamics

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