NASA NTRS · 19680027315
Optimal guidance from hyperbolic to circular orbits
Abstract
Solution for minimum fuel guidance from hyperbolic to circular orbit
Keep this discovery
Explore connections, maps & timelines
Edelbaum, T. N.. 1968-01-01. Optimal guidance from hyperbolic to circular orbits. https://ntrs.nasa.gov/citations/19680027315
Cite the original work for its findings. Save a collection to share your selection of sources.