AERSP 309 was a junior-level Astronautics course that covered 3D kinematics, rigid-boy dynamics, orbits, and orbital maneuvers. There were several projects and assignments that required Matlab to develop solutions to problems related to the course topics. 

Projects included: 

• Writing a script that converts a satellite’s position and velocity from its own reference frame to the Earth’s reference frame 
• Use Matlab to calculate several orbital elements and the three classical orbital angles to evaluate location in the 2D orbital plane 
• Use of Euler Parameters to describe reference frame orientation 
• Given limited orbital element information, find the rest of the data