Optimal time re-entry of vehicles by asymptotic matching

Author:

Sero-Guillaume O.1,Bernardin D.1,Felici T.1,Zouaoui D.1,Antonicelli M.2

Affiliation:

1. Centre National de la Recherche Scientifique, 54504 Vandoeuvre les Nancy, France

2. Aerospatiale, Les Mureaux Cedex, 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

Reference8 articles.

1. A new boundary layer matching procedure for singularly perturbed system

2. Optimal Thrust Control with Proportional Navigation Guidance

3. Singular Perturbation Techniques for On-Line Optimal Flight-Path Control

4. 5Kokotovic, P., Khalil, H. K., and O'Reilly, J., Singular Pertubation Methods in Control: Analysis and Design, Academic, New York, 1986, pp.279-287.

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2. Entry Trajectory Optimization with Analytical Feedback Bank Angle Law;AIAA Guidance, Navigation and Control Conference and Exhibit;2008-06-15

3. Singular Perturbations and Time Scales in Guidance and Control of Aerospace Systems: A Survey;Journal of Guidance, Control, and Dynamics;2001-11

4. Asymptotic matching and genetic optimization applied to optimal aerospace design;International Journal of Systems Science;1997-03

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