NASA NTRS · 19670007468
Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude
Abstract
Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude
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Bryson, A. E., Jr., Winfield, D. H.. 1966-07-01. Nonlinear feedback solution for minimum-time injection into circular orbit with constant thrust acceleration magnitude. https://ntrs.nasa.gov/citations/19670007468
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