C++ implementation of EKF_GEOS3, an Extended Kalman Filter for GEOS-3 satellite orbit determination. Features custom matrix algebra, JPL DE430 ephemerides, IERS corrections, and full astrodynamics modeling.
cpp astrodynamics aerospace scientific-computing academic-project numerical-integration kalman-filter matrix-algebra orbit-determination satellite-navigation jpl-ephemeris geos-3 iers-corrections
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Updated
Nov 4, 2025 - C++