Numerical computation of optimal trajectories for coplanar, aeroassisted orbital transfer

DOI10.1023/A:1026454013374zbMath1168.49310OpenAlexW1486974859MaRDI QIDQ1841566

H. J. Oberle, H. Baumann

Publication date: 18 February 2001

Published in: Journal of Optimization Theory and Applications (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1023/a:1026454013374

zbMATH Keywords

minimum principleoptimal control theorymultiple shooting techniquesaeroassisted orbital transfer

Mathematics Subject Classification ID

Applications of optimal control and differential games (49N90) Application models in control theory (93C95) Optimality conditions for problems involving ordinary differential equations (49K15)

Related Items (4)

3D geosynchronous transfer of a satellite: Continuation on the thrust ⋮ Operations research in the space industry ⋮ Using Lie symmetry analysis to solve a problem that models mass transfer from a horizontal flat plate ⋮ Une approche géométrique du contrôle optimal de l'arc atmosphérique de la navette spatiale

Uses Software

• BNDSCO

Cites Work

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• Properties of the optimal trajectories for coplanar, aeroassisted orbital transfer
• Existence and multiple solutions of the minimum-fuel orbit transfer problem
• Optimal trajectories for aeroassisted orbital transfer

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