Historical Build Log

End-to-end mission flow diagram
Part 5Log ID · #005
Software

From Preparation to Mission Output: End-to-End Flow

How flight planning, target search, mapping, operator approval, and payload delivery join one mission chain.

Quadcopter first flight tests
Part 4Log ID · #004
Avionics

Aviation Electronics: First Step into the Real World

Comprehensive ground tests, then first flight — sensor calibration, motor and failsafe checks, and PID tuning brought our quadcopter to stable, reliable flight.

Map mosaic generated from a data set
Part 4Log ID · #004
Software

From Individual Images to a Usable Map

Distance-based image collection, parallel processing pipelines, and a mosaic-generation approach developed with a data set.

Power distribution board wiring
Part 3Log ID · #003
Avionics

Aviation Electronics: Giving Life to the UAV

With mechanics done, we moved to electronics — a central PDB, tidy soldered wiring, a vibration-damped Pixhawk, the mission computer, and carefully placed GPS and telemetry.

Target detection on an aerial image
Part 3Log ID · #003
Software

From a Single Image to a Safe Delivery Decision

How onboard target detection, geolocation, operator verification, and the planned controlled-payload mechanism work together.

Motor selection for the quadcopter
Part 2Log ID · #002
Avionics

Aviation Electronics: Choosing the UAV's Muscles

Reinforcements nudged our MTOW up, so we compared two KV280 motors — T-Motor MN701-S vs the fully integrated Hobbywing X6-SE — and picked the sealed, all-in-one X6-SE.

Motor arms and landing gear assembly
Part 2Log ID · #002
Manufacturing

Manufacturing Logs 2

Cured parts came out of the mould, trimmed and drilled for joints and cabling. Aviation-grade carbon tubes were cut to spec for the motor arms and landing gear — frame ready for avionics.

Avionics components
Part 1Log ID · #001
Avionics

Aviation Electronics

We started with the brain, not the wings — scoping the minimum-requirement components and testing salvageable parts from past prototypes.

Optimized airframe after FEA iteration
Part 4Log ID · #004
Design Analyze

Design Iteration & Optimization

The FEA flagged high stresses where the carbon arms meet the body under hard landings. We filleted corners, reinforced the joints, trimmed weight — then re-ran the analysis to confirm safe margins.

Ground Control Station interface
Part 2Log ID · #002
Software

Mission Control on the Ground: The Ground Control Station

How a Python- and PyQt6-based GCS combines telemetry, mission planning, safety, and operator decisions in one interface.

Carbon fiber body manufacturing
Part 1Log ID · #001
Manufacturing

Manufacturing Logs 1

From design to the workshop — a 3D-printed PLA plug, a carbon fiber mould, an angled ply layup with fiberglass reinforcements, and a vacuum-bagged cure.

FEA analysis of the drone airframe
Part 3Log ID · #003
Design Analyze

Analysis Logs

Our 3D model looked flawless on screen — but virtual has no gravity, wind, or vibration. The analysis team meshed the drone in ANSYS and ran the flight-load simulations.

System data flow architecture diagram
Part 1Log ID · #001
Software

Bringing an Autonomous Mission Together as One System

An architecture for SUAS 2026 that connects the camera, mission computer, flight control, telemetry, and operator decisions.

Quadcopter CAD model — X configuration
Part 2Log ID · #002
Design Analyze

Mission Analysis & Mechanical Design 2

We selected the quadcopter concept for SUAS 2026 and moved into CAD — an X configuration, electronics packaging, and a balanced center of gravity for a modular, serviceable airframe.

Part 1Log ID · #001
Design Analyze

Mission Analysis & Mechanical Design

From a blank page to the skies — before any 3D software, we defined the mission, questioned what the aircraft must do, and picked a concept with a decision matrix.