To predict the performance of the VDS and the launch vehicle, I developed a simulation in MathWorks Simulink.
It is used primarily as a test bed for experimental GNC algorithms and avionics configurations, and it also allows mission performance prediction with customizable weather scenarios, 6DOF equations of motion, and launch animation.
The simulation also supported learning and predictive apogee targeting algorithm experiments.
Future improvements included a higher-fidelity aerodynamic model and hardware-in-the-loop capabilities.