APPLICATION OF BIFURCATION METHODS TO NONLINEAR FLIGHT DYNAMICS PROBLEMS

Authors
GOMAN MG ZAGAINOV GI KHRAMTSOVSKY AV
Citation
Mg. Goman et al., APPLICATION OF BIFURCATION METHODS TO NONLINEAR FLIGHT DYNAMICS PROBLEMS, Progress in aerospace sciences, 33(9-10), 1997, pp. 539-586
Citations number
65
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
Progress in aerospace sciences → ACNP
ISSN journal
03760421
Volume
33
Issue
9-10
Year of publication
1997
Pages
539 - 586
Database
ISI
SICI code
0376-0421(1997)33:9-10<539:AOBMTN>2.0.ZU;2-L
Abstract
Applications of global stability and bifurcational analysis methods ar e presented for different nonlinear flight dynamics problems, such as roll-coupling, stall, spin, etc. Based on the results for different re al aircraft, F-4, F-14, F-15, High Incidence Research Model, (HIRM), t he general methods developed by many authors are presented. The outlin e of basic concepts and methods from dynamical system theory are also introduced. (C) 1997 Elsevier Science Ltd.