Differential Equations and Nonlinear Mechanics
Volume 2009 (2009), Article ID 842656, 26 pages
doi:10.1155/2009/842656
Research Article

Oscillation Susceptibility Analysis of the ADMIRE Aircraft along the Path of Longitudinal Flight Equilibriums in Two Different Mathematical Models

1Faculty of Mathematics and Computer Science, West University of Timisoara, Bulv. V.Parvan 4, 300223 Timisoara, Romania
2Faculty of Physics, West University of Timisoara, Bulv. V.Parvan 4, 300223 Timisoara, Romania
3Institute for Theoretical and Experimental Analysis of Aeronautical Structures, STRAERO, Bd.Iuliu Maniu 220, 061126, Bucharest, Romania

Received 8 March 2009; Revised 3 May 2009; Accepted 28 June 2009

Academic Editor: Nicola Bellomo

Copyright © 2009 Stefan Balint et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

Linked References

  1. R. K. Mehra and R. K. Prasanth, “Bifurcation and limit cycle analysis of nonlinear pilot induced oscillations,” in Proceedings of the AIAA Atmospheric Flight Mechanics Conference and Exhibit, Boston, Mass, USA, August 1998, AIAA-1998-4249.
  2. Unified Pilot-Induced Oscillation Theory, vol. 1–4, Wright-Patterson AFB, Ohio, 1996, WL-TR-96.
  3. B. A. Kish, et al., “A limited flight test investigation of pilot-induced oscillation due to rate limiting,” in Proceedings of the AIAA Guidance, Navigation, and Control Conference, New Orleans, La, USA, August 1997, AIAA Paper 97-3703.
  4. D. H. Klyde, D. T. McRuer, and T. T. Myers, “Pilot-induced oscillation analysis and prediction with actuator rate limiting,” Journal of Guidance, Control, and Dynamics, vol. 20, no. 1, pp. 81–89, 1997. View at Publisher · View at Google Scholar
  5. R. K. Mehra, et al., “Global stability and control analysis of aircraft at high angles of attack,” Tech. Rep. ONR-CR215-248, 1977.
  6. A. Ionita and A. Halanay, “Delay induced oscillations,” in Proceedings of the AIAA Atmospheric Flight Mechanics Conference, New Orleans, La, USA, August 1997, AIAA-97-3502.
  7. J. S. Shamma and M. Athans, “Guaranteed properties of gain scheduled control for linear parameter-varying plants,” Automatica, vol. 27, no. 3, pp. 559–564, 1991. View at Zentralblatt MATH · View at MathSciNet
  8. B. Etkin and L. Reid, Dynamics of Flight: Stability and Control, John Wiley & Sons, New York, NY, USA, 1996.
  9. M. Cook, Flight Dynamics Principles, John Wiley & Sons, New York, NY, USA, 1997.
  10. St. Balint, A. M. Balint, and A. Ionita, vol. 22, no. 4, 2009, Journal of Aerospace Engineering. In press.
  11. J. Guckenheimer and P. Holmes, Nonlinear Oscillations, Dynamical Systems, and Bifurcations of Vector Fields, vol. 42 of Applied Mathematical Sciences, Springer, New York, NY, USA, 1983. View at MathSciNet
  12. Y. A. Kuznetsov, Elements of Applied Bifurcation Theory, vol. 112 of Applied Mathematical Sciences, Springer, New York, NY, USA, 2nd edition, 1998. View at MathSciNet
  13. E. Kaslik and S. Balint, “Structural stability of simplified dynamical system governing motion of ALFLEX reentry vehicle,” Journal of Aerospace Engineering, vol. 20, no. 4, pp. 215–219, 2007. View at Publisher · View at Google Scholar
  14. Ş. Balint, L. Brăescu, and E. Kaslik, Regions of Attraction and Applications to Control Theory, vol. 1 of Mathematical Problems in Engineering and Aerospace Sciences, Cambridge Scientific, Cambridge, UK, 2008. View at MathSciNet