NASA NTRS · 19680034315
Trajectory computation by a hybrid computer for the Apollo midcourse abort simulation.
Abstract
Hybrid computer simulation for Apollo midcourse guidance from elliptical preabort orbit to another ellipse, using coplanar/noncoplanar orbit change guidance scheme
Keep this discovery
Explore connections, maps & timelines
Smith, C. L.. 1967-08-01. Trajectory computation by a hybrid computer for the Apollo midcourse abort simulation.. https://ntrs.nasa.gov/citations/19680034315
Cite the original work for its findings. Save a collection to share your selection of sources.