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Created a full Attitude Determination and Control Architecture to meet design requirements for Simulated Clearspace-1 Mission (AA279C, Stanford Uniersity)

Replicated the Lucy trajectory by piecing together lamberts solutions (AA279B, Stanford University)

Coded a differential GPS routine in python that simulated and analyzed the achievable accuracies using different GPS module baseline configurations (AA272, Stanford University)

Recreated the InSight trajectory and analyzed mission design properties such as RLA, DLA, C3 etc (AA279B, Stanford University)

Optimized transfer trajectory for minimum fuel using burn cost burn trajectory (AERO557, Cal Poly SLO)