NASA NTRS · 19640011039
An optimal guidance approximation theory
Abstract
Optimal guidance approximations using perturbation theory
Explore related subjects
Keep this discovery
Explore connections, maps & timelines
Kelley, H. J.. 1964-03-17. An optimal guidance approximation theory. https://ntrs.nasa.gov/citations/19640011039
Cite the original work for its findings. Save a collection to share your selection of sources.