projects
Attitude Dynamics and Control of a Rigid Spacecraft in LEO
Quaternion simulation, gravity-gradient torque, and PD stabilization in MATLAB.
EUREKA Rocket Launch Team – LASERHAWK Competition Rocket
Programming lead for avionics and data logging systems on a 5-foot competition rocket that won 1st place at the 2024 NSBE National Convention Boeing Rocket Launch Competition
Vision-Generative Assurance for Spacecraft Rendezvous and Proximity Operations
AIAA SciTech 2027 research project on assurance-centered generative autonomy for spacecraft RPO.
ESA SPARK 2026 – Spacecraft Detection and Segmentation
Deep learning pipeline for spacecraft classification and semantic segmentation in synthetic orbital imagery
Parrot Mambo Quadcopter Control
Experimental dynamics and control project using MATLAB/Simulink to model, simulate, and implement attitude control on a Parrot Mambo quadcopter.
Space Debris Detection for Orbital Scene Awareness
YOLOv8-based object detection model for identifying debris and satellites in synthetic orbital imagery
Mixture-Ratio Sensitivity of a Hydrogen–Oxygen Rocket Engine Using NASA CEA
How Tc and Isp change with O/F for GH2/GO2 at 68 atm, restricted vs full equilibrium chemistry
Development of a 6 Degrees of Freedom (6DOF) Flight Dynamics Model for the Airbus A320
MATLAB-based rigid-body flight dynamics model capturing full translational and rotational aircraft motion
Light Intensity Measurement & Validation of Radiative Laws
Experimental validation of the inverse-square law and Lambert’s cosine law using Arduino sensing and MATLAB analysis.
Finite Element Structural Analysis Using Simcenter Femap with NASTRAN
Static structural analysis of beam and rod elements with validation against analytical solutions
Wind Tunnel Aerodynamic Testing of a Space Shuttle Orbiter Scale Model
Low-speed wind tunnel testing of a 1:286 scale Space Shuttle Orbiter with lift and drag measurements across angle of attack
Experimental Boundary Layer Analysis Using Hot-Wire Anemometry
Turbulent flat-plate boundary layer characterization using hot-wire measurements, FFT analysis, and comparison with classical theory
AI-Driven Collision Avoidance for Crowded Orbital Environments
Artificial intelligence methods for conjunction screening, uncertainty modeling, and autonomous maneuver planning in LEO