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Showing 1 to 1 of 1 for “"Thrust-acceleration-squared optimal"”.
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Spacecraft trajectory optimization using many embedded Lambert problems
… short arcs simultaneously approximate low thrust and eliminates the need to know the structure of a high-thrust impulsive-maneuver solution. A set of examples show the EBVP technique to be efficient, robust, and useful. In particular, an example using 256 revolutions, 6143 segments, and a …