NASA NTRS · 19670005096
Theoretical basis for the Double Precision Orbit Determination Program /DPODP/. III - Probe trajectory
Abstract
Differential motion equations of probe numerically integrated in rectangular coordinate system for probe ephemeris
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Moyer, T. D.. 1966-09-30. Theoretical basis for the Double Precision Orbit Determination Program /DPODP/. III - Probe trajectory. https://ntrs.nasa.gov/citations/19670005096
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