Systems engineered a payload using an Arduino microcontroller, transmitter & receiver modules, ESP32-camera, and a servo motor

Following the V-model, stakeholder requirements, design constraints,  budget and project timeline were defined.

The design was tested against the outlined requirements and satisfied all criteria.

Designed, modelled, and assembled gearbox for battle robot using CATIA V5 based on client requirements

Created engineering drawings for each part to showcase dimensioning & GD&T compliance

Conducted stress analysis of individual parts to ensure compliance with design objective

Performed XFLR5 analysis of wing and empennage iteration for VLJ design iteration

Analyzed airfoil characteristics of wing and empennage under key phases of flight: takeoff and landing

The aircraft's aerodynamics met FAR23 requirements and were successfully integrated with other components to achieve the required mission objectives

Designed inlet geometry for a fictional supersonic engine to travel between New York and London

Rendered inlet geometry in MATLAB for a set of given inlet conditions of Mach 3.2, three shocks, and upstream normal shock of 1.3

Computed Mach numbers, deflection angles, and shock angles across each shockwave using parametric analysis and Oswatitsch’s Principle

Object masked a motherboard image in Python using OpenCV to isolate key features,  bolstering model recognition

Trained YOLOv8n computer vision model for PCB component identification to streamline manufacturing verification processes

Model designed to achieve a high accuracy while maintaining less than 200 epochs and an image size greater than 900

Performed engineering analysis on an airfoil with flaps at three different settings: 0%, 50%, and 100%

Modelled and assembly of airfoil flap mechanism using CATIA V5 and simulated using DMU Kinematics

Minimized volume required to deploy flap mechanism through iterative design