Atmospheric reentry hemisphere prediction for prograde orbits using logical disjunction
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DOI: 10.1016/j.asr.2021.01.056
Abstract: Abstract A unique logic-based algorithm for atmospheric reentry hemisphere prediction is presented for spacecraft in low-eccentricity, prograde low Earth orbits at altitudes of 300 km and lower. Using two-line element (TLE) data for initial orbit conditions,… read more here.
Keywords: hemisphere prediction; reentry hemisphere; logical disjunction; atmospheric reentry ... See more keywords