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Oscillation susceptibility analysis of the ADMIRE aircraft along the path of longitudinal flight equilibrium
by
Stefan Balint
West University of Timisoara, Department of Computer Science, Timisoara, RO 300223
Coauthors: Agneta M. Balint (West University of Timisoara, Department of Physics)
Achim Ionita (Institute for Theoretical and Experimental Analysis of Aeronautical Structures, Bucharest)
In this paper the oscillation susceptibility of the ADMIRE aircraft along the path of longitudinal flight equilibriums is analyzed in the general and in a simplified flight model. The stability of the equilibriums and the existence of Hopf bifurcations and saddle nodes bifurcations is researched. The behavior of the aircraft is simulated in both models. The differences between the results obtained in the models are discussed.
Date received: March 5, 2008
Copyright © 2008 by the author(s). The author(s) of this document and the organizers of the conference have granted their consent to include this abstract in Atlas Conferences Inc. Document # caub-64.