Uploaded November 2016 | Updated September 2026, 5 hours ago

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Hello!

This is my second Simulink project. Real thrust data was obtained from the Shuttle as well as mass, and the equations of motion for a rigid body launch vehicle were modeled in MATLAB.

The equations of motion are solved using Euler's method with relevant initial conditions. The resulting trajectory was exported from the MATLAB m. file, imported into Simulink, and plotted in FlightGear.

I will be making a tutorial on how to use FlightGear and how to link it to MATLAB.

Thank you for watching!

Vin

My Instagram: instagram.com/vinayak_desh
My Website: vinayakd.com