NASA NTRS · 19700030196
Optimal three dimensional reentry trajectories for Apollo-type vehicles
Abstract
Numerical optimization method based on perturbation theory for calculating optimal three dimensional reentry trajectories for Apollo type vehicles
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Williamson, W. E., Jr.. 1970-01-01. Optimal three dimensional reentry trajectories for Apollo-type vehicles. https://ntrs.nasa.gov/citations/19700030196
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