NASA NTRS · 19660058101
Powered flight trajectory optimization for lunar and interplanetary transfer.
Abstract
Steepest descent method of trajectory optimization for computing lunar and interplanetary transfer missions, noting terminal constraints
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Chuck, W., Rosenbaum, R., Willwerth, R. E.. 1966-04-01. Powered flight trajectory optimization for lunar and interplanetary transfer.. https://ntrs.nasa.gov/citations/19660058101
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