Application of continuation and bifurcation methods to the design of control systems-Reference-Cited by-同舟云学术

Application of continuation and bifurcation methods to the design of control systems

Published:1998-10-15 Issue:1745 Volume:356 Page:2277-2295
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:

Goman M. G.¹²,Khramtsovsky A. V.¹

Affiliation:

1. Central Aerohydrodynamic Institute (TsAGI), Zhukovsky 140160, Russia

2. Department of Mathematical Sciences, Faculty of Computing Science and Engineering, De Montfort University, Leicester LE1 9BH, UK

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

Link

https://royalsocietypublishing.org/doi/pdf/10.1098/rsta.1998.0274

Reference30 articles.

1. Robust flight control design using dynamic inversion and structured singular value synthesis

2. AGARD 1990 Rotary-balance testing for aircraft dynamics. AGARD Advisory Report no. 265.

3. Bifurcation Analysis of Nonlinear Aircraft Dynamics

4. Cobleigh B. R. Croom M. A. & Tamrat B. F. 1994 Comparison of X-31 flight wind-tunnel and water-tunnel yawing moment asymmetries at high angles of attack. High Alpha Conference IY: Electronic Workshop NASA Dryden Flight Research Center 12-14 July 1994 Paper HA-AERO-06. URL: http://www.dfrf.nasa.gov/Workshop/HighAlphaIV/highalpha.html.

5. Doedel E. & Kernevez J. P. 1986 AUTO: Software for continuation and bifurcation problems in ordinary differential equations. California Institute of Technology Pasadena.

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