NASA NTRS · 19680057715
Trajectory optimization using regularized variables.
Abstract
Trajectory optimization of space vehicle with continuous thrust based on regularized equations, comparing perturbation method for earth-Jupiter rendezvous transfer
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Lewallen, J. M., Szebehely, V., Tapley, B. D.. 1968-09-01. Trajectory optimization using regularized variables.. https://ntrs.nasa.gov/citations/19680057715
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