A Simulink project which can accurately simulate the motion of a flying rocket in one-dimensional space.

A 2D simulation of orbital mechanics and rocket launch from earth

6-DoF Rocket Simulator

6-DOF rocket trajectory optimization. Find pitch program coefficients (a, b, c) to reach 200 km apogee using fsolve shooting method. Features: - Quaternion-based attitude dynamics - Exponential atmosphere model - Quadratic drag - Mass depletion - FSOLVE parameter optimization - Full 3D visualization Topics: fsolve, ode45, quaternions

Task I made for course Orbital Mechanics during the Space Applications Masters program study