NASA NTRS · 19680033017
Real-time optimal guidance.
Abstract
Repetitive in-flight calculation of optimal rocket guidance using algorithm method for solving boundary value problem
Keep this discovery
Explore connections, maps & timelines
Brown, K. R., Johnson, G. W.. 1967-10-01. Real-time optimal guidance.. https://ntrs.nasa.gov/citations/19680033017
Cite the original work for its findings. Save a collection to share your selection of sources.