Optimal multiple-impulse satellite evasive maneuvers

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DOI10.2514/3.21239zbMath0806.70019OpenAlexW2056525328MaRDI QIDQ4307984

John E. Prussing, Ronald S. Clifton

Publication date: 16 February 1995

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

Full work available at URL: https://doi.org/10.2514/3.21239

zbMATH Keywords

fuel minimization rendezvous with orbit station three-impulse solutions two-impulse free-return trajectories

Mathematics Subject Classification ID

Orbital mechanics (70M20)

Related Items (2)

Closed-form solution of an idealized, optimal, highly eccentric hyperbolic rendezvous problem ⋮ Optimal impulsive ellipse-to-circle coplanar rendezvous

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