Czasopismo
2006
|
Vol. 18, iss. 1
|
71-86
Tytuł artykułu
Autorzy
Wybrane pełne teksty z tego czasopisma
Warianty tytułu
Kontynuacyjna metoda badania nieliniowej dynamiki samolotu supermanewrowego
Języki publikacji
Abstrakty
This paper describes the implementation of continuation methods and bifurcation analysis in the "global" identification of an agile aircraft dynamics. In the examples presented, it integrates features of eigenstructure methods within the nonlinear state-parameter environment. The basis of the continuation analysis is outlined and demonstrated using a highly nonlinear aircraft model.
W pracy opisano zastosowanie metod kontynuacyjnych i analizy bifurkacyjnej do "globalnej" identyfikacji dynamiki lotu samolotu supermanewrowego. Przedstawiono cechy sprzężeń zwrotnych pozwalających na osiągnięcie założonej struktury wartości własnych, w zakresie nieliniowości parametrów stanu.
Słowa kluczowe
Czasopismo
Rocznik
Tom
Strony
71-86
Opis fizyczny
Bibliogr. 19 poz., rys.
Twórcy
autor
autor
- Instytut Techniczny Wojsk Lotniczych, 01-494 Warszawa, ul. Księcia Bolesława 6
Bibliografia
- 1. AGARD FMP WG 19. Operational agility. AGARD Adv Rpt 314, Apr 1994.
- 2. Avanzini G., De Matteis G.: Bifurcation Analysis of a Highly Augmented Aircraft Model. Journal of Guidance, Control & Dynamics, Vol. 20, No. l, 1998.
- 3. Carroll J. V. AGARD FMP WG 19. Operational agility. AGARD Adv Rpt 314, Apr 1994.
- 4. Charles G. A. et. all.: Aircraft Flight Dynamics Analysis and Controller Design Using Bifurcation Tailoring. AIAA Guidance, Navigation and Control Conference Technical Papers, USA, 2002. AIAA-2002-4751-CP, American Institute of Aeronautics and Astronautics.
- 5. Ermentrout B.: Simulating, Analyzing, and Animating Dynamical Systems. A Guide to XPPAUT for Researchers and Students, SIAM, Philadelphia, 2002.
- 6. Goman M. G., Khramtsovsky A. V Application of continuation and bifurcation methods to the design of control systems. Phil. Trans. R. Soc., No. A 356, London, 1998, p. 2277-2295.
- 7. Seydel R.: Practical Bifurcation and Stability Analysis: From Equilibrium to Chaos. Springer Verlag, 1994.
- 8. Guckenheimer J., Holmes J.: Nonlinear Oscillations, Dynamical Systems, and Bifurcations of Vector Fields. Springer-Verlag, New York, 1983.
- 9. Guicheteau P.: Bifurcation Theory: a Tool for Nonlinear Flight Dynamics. Phil. Trans. R. Soc., No. A 356, London, 1998, p 2181-2201.
- 10. Ioos G., Joseph D.: Elementary Stability and Bifurcation Theory. Springer-Verlag, New York, 1980.
- 11. Jahnke C. C., Culick F. E. C.: Application of Bifurcation Theory to the High-Angle-of-Attack Dynamics of the F-14. Journal of Aircraft, Vol. 31, No. 1, 1994, p. 26-34.
- 12. Littleboy D. M., and Smith P. R.: Using bifurcation methods to aid nonlinear dynamic inversion control law design. J. Guidance, Navigation and Control, Vol. 21, No. 4, 1998, p. 632-638.
- 13. Lowenberg M. H.: Bifurcation Analysis of Multiple-Attractor Flight Dynamics. Phil. Trans. R. Soc., No. A 356, London, 1998, p. 1745:2297-2319.
- 14. Marusak A. J., Pietrucha J. A., Sibilski K. S.: Prediction of Aircraft Critical Flight Regimes Using Continuation and Bifurcation Methods, 38th Aerospace Sciences Meeting Technical Papers, USA, 2000, AIAA-2000-0976-CP, American Institute of Aeronautics and Astronautics.
- 15. Sibilski K.: An Agile Aircraft Non-Linear Dynamics by Continuation Methods and Bifurcation Theory. ICAS-2000-712, Proceedings of 22nd ICAS Congress, Harrogate, UK, 2000.
- 16. Sinha N. K., Ananthkrishnar N.: Use of the Extended Bifurcation Analysis Method for Flight Control Law Design. 40th AIAA Aerospace Sciences Meeting, USA, 2002, AIAA-2002-0249-CP, American Institute of Aeronautics and Astronautics.
- 17. Troger H., Steindl A.: Nonlinear Stability and Bifurcation Theory. Springer-Verlag, New York, 1991.
- 18. Van Patten R.: Supermaneuverability and Superagility. Aeromedical and Training Digest, Vol. 7 No.l,January 1993.
- 19. Wiggins S.: Introduction to Applied Non-linear Dynamical Systems and Chaos. Springer-Verlag, New York, 1990.
Typ dokumentu
Bibliografia
Identyfikatory
Identyfikator YADDA
bwmeta1.element.baztech-article-BPZ3-0021-0005