System design impact of guidance and navigation analysis for a SEPS 1979 Encke flyby

Details System design impact of guidance and navigation analysis for a SEPS 1979 Encke flyby System design impact of guidance and navigation analysis for a SEPS 1979 Encke flyby

Aug 1975

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1975fmet.symp..182h&link_type=abstract

In NASA. Goddard Space Flight Center Flight Mech./Estimation Theory Symp. p 182-190 (SEE N76-10167 01-12)

Computer Science

Comets, Flyby Missions, Satellite Guidance, Trajectory Control, Error Analysis, Orbital Mechanics, Solar Orbits, Solar Propulsion

Scientific paper

Baseline guidance and navigation strategy for an ecliptic projection of
the Encke flyby mission consider solar electric propulsion stage
parameters in generating optimized and targeted trajectory control.
Results show the Encke relative approach error to be dominated by
ephemerical uncertainties, particularly the velocity components.

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