NASA NTRS · 19650026535
A trajectory optimization technique based upon the theory of the second variation
Abstract
Approximation method using Euler-Lagrange equation for trajectory optimization
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Kelley, H. J., Kopp, R. E., Moyer, H. G.. 1964-07-01. A trajectory optimization technique based upon the theory of the second variation. https://ntrs.nasa.gov/citations/19650026535
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