Numerical Study of Optimal Trajectories with Singular Arcs for an Ariane 5 Launcher
Author:
Affiliation:
1. Institut National de Recherche en Informatique et en Automatique, 78153 Rocquencourt Cedex, France
2. Centre National d’Etudes Spatiales, 91023 Evry Cedex, France
3. Universite d’Orleans, 45067 Orleans Cedex 2, France
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
http://arc.aiaa.org/doi/pdf/10.2514/1.37387
Reference11 articles.
1. Goddard problem in presence of a dynamic pressure limit
2. Optimization of Launch Vehicle Ascent Trajectories with Path Constraints and Coast Arcs
3. Closed-Loop Endoatmospheric Ascent Guidance
4. A Generalized Legendre-Clebsch Condition for the Singular Cases of Optimal Control
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