NASA NTRS · 19710030891
A linear algorithm for determining relative orbital state using angle data
Abstract
Linear algorithms for determining spacecraft relative orbital state using angle data with digital computer
Keep this discovery
Explore connections, maps & timelines
Schneider, A. M.. 1970-11-01. A linear algorithm for determining relative orbital state using angle data. https://ntrs.nasa.gov/citations/19710030891
Cite the original work for its findings. Save a collection to share your selection of sources.