mattwernerr/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.

MATLABStars 7Forks 1Watchers 7Open issues 6
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Ownermattwernerr
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Last pushed2024-06-13
Last updated2025-12-15
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