NASA NTRS · 19680063324
Optimal guidance with transition partial derivative matrices.
Abstract
Newton method for boundary value problem associated with differential equations applied to Lambert, rendezvous and orbital transfer problems
Keep this discovery
Explore connections, maps & timelines
Ingram, H. L.. 1968-10-01. Optimal guidance with transition partial derivative matrices.. https://ntrs.nasa.gov/citations/19680063324
Cite the original work for its findings. Save a collection to share your selection of sources.