A simple targeting technique for two-body spacecraft trajectories

DOI10.2514/3.20062zbMATH Open0607.93031OpenAlexW2045202916MaRDI QIDQ3748147

Dale Gordon Stuart

Publication date: 1986

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

Full work available at URL: https://doi.org/10.2514/3.20062

zbMATH Keywords

targetingguidance algorithmorbital boundary-value problemtwo-body, space-flight guidance problems

Mathematics Subject Classification ID

Numerical optimization and variational techniques (65K10) Orbital mechanics (70M20) Control/observation systems governed by ordinary differential equations (93C15)

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