Optimal aerodynamic control by matched asymptotic expansions-Reference-Cited by-同舟云学术

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Optimal aerodynamic control by matched asymptotic expansions

Published:1976-05 Issue:5-6 Volume:3 Page:319-332
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Frostic Fred,Vinh Nguyen X.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference4 articles.

1. Solution of the exact equations for three-dimensional atmospheric entry using directly matched asymptotic expansions;Busemann;NASA Report,1975

2. Contribution à l'étude schématique des trajectoires semi-ballistique à grande portée;Contensou,1965

3. Matched asymptotic solutions for optimum lift controlled atmospheric entry;Shi;AIAA J.,1971

4. Optimum three-dimensional atmospheric entry;Vinh;Acta Astronautica,1975

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1. Trajectory Optimization and Multiple-Sliding-Surface Terminal Guidance in the Lifting Atmospheric Reentry;Aerotecnica Missili & Spazio;2024-05-25

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

4. The 1st John V. Breakwell Memorial Lecture;Acta Astronautica;1996-05

5. Optimal guidance of aeroassisted transfer vehicles based on matched asymptotic expansions;Journal of Guidance, Control, and Dynamics;1995-07

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