Analysis of Aircraft Nonlinear Dynamics Using Non-Gradient Based Numerical Methods and Attainable Equilibrium Sets
Author:
Affiliation:
1. De Montfort University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2012-4406
Reference11 articles.
1. Application of bifurcation methods to nonlinear flight dynamics problems
2. Level Flight Trim and Stability Analysis Using Extended Bifurcation and Continuation Procedure
3. Evaluation of Aircraft Performance and Maneuverability by Computation of Attainable Equilibrium Sets
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