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Showing 1 to 1 of 1 for “"Flight-time function"”.
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Spacecraft trajectory optimization using many embedded Lambert problems
… 256 revolutions, 6143 segments, and a constant flight time per segment, optimizes in 5.5 hours using a single processor. After this initial demonstration, the EBVP technique is improved by a function which enables variable flight time per segment. Guided by the well-known Sundman transformation, …