Bifurcation analysis of multiple–attractor flight dynamics

Author:

Lowenberg Mark H.1

Affiliation:

1. Department of Aerospace Engineering, University of Bristol, Queens Building, University Walk, Bristol BS8 1TR, UK

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

Reference32 articles.

1. The X-31 aircraft: Advances in aircraft agility and performance

2. Avanzini G. & de Matteis G. 1996 Bifurcation analysis of a highly augmented aircraft model. In Proc. AIAA Atmospheric Flight Mechanics Conf. San Diego CA USA August paper no. AIAA-96-3367-CP pp. 60-68.

3. Bifurcation Analysis of Nonlinear Aircraft Dynamics

4. Doedel E. J. Wang X. & Fairgrieve T. 1994 AUTO94 software for continuation and bifurcation problems in ordinary differential equations. Applied Mathematics Report CALTECH.

5. Goman M. G. & Khramtsovsky A. V. 1995 A review of bifurcation theory methods in nonlinear flight dynamics problems: application to HIRM high angle of attack dynamics. TsAGI Technical Report for Flight Systems Dept. DRA Bedford UK.

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