NASA NTRS · 19680040422
Iteration procedures for indirect trajectory optimization methods.
Abstract
Numerical method solution of nonlinear two point boundary value problem associated with optimum transfer of spacecraft
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Lewallen, J. M., Tapley, B. D., Williams, S. D.. 1968-03-01. Iteration procedures for indirect trajectory optimization methods.. https://ntrs.nasa.gov/citations/19680040422
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