Matt Werner's repositories
rtraj
Simulate the trajectory of a suborbital or ground-to-VLEO rocket using high-fidelity models of Earth's terrain, atmosphere (with wind), and gravitational and magnetic fields by providing the dynamics to determine the rocket's position and orientation (6-DOF) throughout the flight.
CMDS
Context Manager for Dynamical Systems
Language:MATLABMIT000
FILM
Framework for Investigating Lagrange Manifolds
Language:MATLAB000
HokieNav-Orbit
Simulate the orbital motion for a CubeSat (HokieNav) as part of a senior design project with VT's ECE department sponsored by The Aerospace Corporation.
LS-Particle-Modeling
Simulate the stochastic motion of a particle in a Lagrangian flow.
photon-geodesics
Calculate the trajectory of a photon passing near a weak Newtonian field using the linearized Einstein field equations.