NASA NTRS · 19730000012
N-body U and K matrix program
Abstract
Computer program was devised to compute free-fall trajectories of satellites, allowing for injection errors and midcourse velocity perturbations. Program consists of trajectory perturbing program and N-body integrating conic program which can also be used as 2-body patch conic program.
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Setter, R. N., Ojeda, L., Hoeft, R. F.. 1973-03-01. N-body U and K matrix program. https://ntrs.nasa.gov/citations/19730000012
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