NASA NTRS · 19710062303
A general branched trajectory optimization algorithm with applications to space shuttle vehicle mission design
Abstract
Branched trajectory optimization algorithm using steepest descent method applied to space shuttle vehicle mission design
Keep this discovery
Explore connections, maps & timelines
Rozendaal, H. L.. 1971-08-01. A general branched trajectory optimization algorithm with applications to space shuttle vehicle mission design. https://ntrs.nasa.gov/citations/19710062303
Cite the original work for its findings. Save a collection to share your selection of sources.