Python package (with C++ base) to compute satellite remote-sensing related orbit data.
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Updated
Sep 17, 2024 - C++
Python package (with C++ base) to compute satellite remote-sensing related orbit data.
N-body space simulator that uses the Runge-Kutta 4 numerical integration method to solve two first order differential equations derived from the second order differential equation that governs the motion of an orbiting celestial. Also has preset demos for two-body and three-body circular orbits which use parametric equations. Uses the SFML (Simp…
A simple JUCE GUI Application with an approximate model of how objects orbit
Python package (with C++ base) to compute satellite remote-sensing related orbit data.
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