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.
A MATLAB code incorporating the analysis method described by Barrowman (1967) to analyse the aerodynamic properties of a supersonic sounding rocket.
Calculation utility programs for various rocket features and properties.
Trajectory Optimization Tool v1.0.10
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