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Fuel-optimal maneuvers of a spacecraft relative to a point in circular orbit

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Publication:3343859
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DOI10.2514/3.19917zbMath0551.93034OpenAlexW2065507881MaRDI QIDQ3343859

Thomas E. Carter

Publication date: 1984

Published in: Journal of Guidance, Control, and Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.2514/3.19917


zbMATH Keywords

circular orbitComputer simulationsrendezvous problemsFuel-optimal maneuvers


Mathematics Subject Classification ID

Linear systems in control theory (93C05) Existence of optimal solutions belonging to restricted classes (Lipschitz controls, bang-bang controls, etc.) (49J30) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15)


Related Items

Singular fuel-optimal space trajectories based on linearization about a point in circular orbit ⋮ Symmetry properties of optimal relative orbit trajectories ⋮ Robust tracking control for rendezvous in near-circular orbits ⋮ Optimal impulsive space trajectories based on linear equations ⋮ Optimal bounded-thrust space trajectories based on linear equations



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