NASA NTRS · 19690039581
Trajectory optimization by a direct descent process.
Abstract
Space vehicle trajectory optimization using computerized step by step steepest descent to minimum cost, considering cost gradient vs control
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Fogarty, L. E., Howe, R. M.. 1968-01-01. Trajectory optimization by a direct descent process.. https://ntrs.nasa.gov/citations/19690039581
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