NASA NTRS · 19680063320
A method for determining optimal fixed-time, N-impulse trajectories between arbitrarily inclined orbits.
Abstract
Optimal fixed time N impulse trajectory determination between inclined orbits using primer vector theory method
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Jezewski, D. J.. 1968-10-01. A method for determining optimal fixed-time, N-impulse trajectories between arbitrarily inclined orbits.. https://ntrs.nasa.gov/citations/19680063320
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