MISSION ASSURANCE // V&V DIVISION REF: JAN 2026

Project Verification & Validation Archive

Technical documentation and requirements traceability for astronautical engineering systems.

ID: AR-N-BODY-01 VERIFICATION: PASSED

N-Body Orbital Simulation

High-fidelity simulation of gravitational interactions using Runge-Kutta 4th Order integration. Validated against Apollo 11 lunar trajectory data.

VALIDATION: COMPLETED (FLIGHT DATA COMPARE)
LANG: Python | ENV: NumPy, Matplotlib
ID: AR-ADCS-02 VERIFICATION: ONGOING

CubeSat ADCS Controller

Attitude Determination and Control System utilizing B-Dot logic for detumbling. Current phase: Hardware-in-the-Loop (HIL) testing.

VALIDATION: ONGOING (SITL PHASE)
LANG: C++, MATLAB/Simulink | HARDWARE: Raspberry Pi