NASA NTRS · 19700000603
Optimum Multi-Impulse Rendezvous Program
Abstract
OMIRPROGRAM determines optimal n-impulse rendezvous trajectories under the restrictions of two-body motion in free space. Lawden's primer vector theory is applied to determine optimum number of midcourse impulse applications. Global optimality is not guaranteed.
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Glandorf, D. R., Onley, A. G., Rozendaal, H. L.. 1970-12-01. Optimum Multi-Impulse Rendezvous Program. https://ntrs.nasa.gov/citations/19700000603
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