A sensitivity analysis for lunar trajectories

Details A sensitivity analysis for lunar trajectories A sensitivity analysis for lunar trajectories

Aug 1986

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1986asdy.conf..261d&link_type=abstract

IN: Astrodynamics Conference, Williamsburg, VA, August 18-20, 1986, Technical Papers (A86-47901 23-13). New York, American Insti

Astronomy and Astrophysics

Astronomy

Earth-Moon Trajectories, Lunar Trajectories, Sensitivity, Three Body Problem, Equations Of Motion, Error Analysis, Orbital Mechanics, Translunar Injection

Scientific paper

Within the context of the restricted problem of three bodies, the
allowable error in initial velocity and initial position for families of
earth-to-moon trajectories is established. The allowable deviation in
initial speed is between 0.05 meters/s and 50 meters/s. The largest
allowable error in initial position is 3.5 km.

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