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3DOF rocket-Simulation

This is my final project for the "Multivariable linear system control" module. This repo contains a 3DOF (two planar coordinates, one rotational coordinate) simulation of a thrust vectoring vehicle. This repo contains the Simulink dynamics model, a Matlab file with mass properties and my final report.

The Simulation

The translational dynamics were modelled by Newton's Second Law, and the attitude dynamics were modelled by T=Ia. The control scheme is full state feedback designed via pole placement and linearizing the dynamics around a hover.

The vehicle attempts to follow a reference trajectory that contains an ascent, translation, and then landing.

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