Piecewise Polynomial Modeling for Control and Analysis of Aircraft Dynamics Beyond Stall
Author:
Affiliation:
1. ONERA–The French Aerospace Lab, 31055 Toulouse, France
2. French Civil Aviation School, 31055 Toulouse, France
Funder
ONERA -- The French Aerospace Lab
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Applied Mathematics,Electrical and Electronic Engineering,Space and Planetary Science,Aerospace Engineering,Control and Systems Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.G003618
Reference26 articles.
1. Application of bifurcation methods to nonlinear flight dynamics problems
2. Upset Dynamics of an Airliner Model: A Nonlinear Bifurcation Analysis
3. Aircraft Trim Recovery from Highly Nonlinear Upset Conditions
4. Stall Recovery Guidance Algorithms Based on Constrained Control Approaches
5. A Multi-Mode Upset Recovery Flight Control System for Large Transport Aircraft
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