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Orbital mechanics and guidance library built on the kOS scriptable flight computer platform. All astrodynamics algorithms are implemented from scratch without black-box solvers.
Core Library (src/core/)
Module
What it implements
orbit.ks
Kepler's equation (Newton-Raphson, elliptic/hyperbolic/near-parabolic), vis-viva, Keplerian element conversions, true/mean anomaly, time-of-flight, Hohmann phase angles, reference frame rotations (TZN, RNP, PQW, inertial) with flight-path-angle corrections for non-circular orbits
node.ks
Maneuver planning: apsis changes at arbitrary true anomaly, orbital plane changes, SOI escape targeting
burn.ks
Tsiolkovsky rocket equation, burn duration with mass depletion, split-burn timing