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CASE STUDY // SYS-MEDRESQValidated System Prototype

MedResQ / Medical Diagnostic & Delivery Drone

Autonomous aerial medical diagnostic and emergency supply payload delivery platform.

#AERIAL#AUTONOMY#AI#PRODUCT_DEVELOPMENT
DEVELOPMENT YEAR2025
MY ROLEEnd-to-End System Design, Flight Firmware & AI Vision Integration
TEAM STRUCTURELead Systems Architect & Robotics Engineer
VALIDATION STATUSValidated System Prototype
THE ENGINEERING PROBLEM

Critical medical supplies and rapid diagnostic telemetry in remote or disaster-stricken terrains often face catastrophic ground transportation delays.

THE ARCHITECTURAL SOLUTION

Engineered an autonomous dual-capability aerial platform equipped with edge computer vision for survivor landing site identification and a drop-mechanism payload bay.

SYSTEM OVERVIEW & ARCHITECTURE

MedResQ integrates PX4 autopilot firmware over MAVLink with a companion computer executing real-time object detection models for autonomous emergency delivery.

SYSTEM ARCHITECTURE BLOCK DIAGRAM FLOW:
Companion Computer (Raspberry Pi/Jetson) ←[MAVLink]→ PX4 Flight Controller → ESCs & Actuators. Edge CV models detect landing markers and release diagnostic packages dynamically.
KEY TECHNICAL HIGHLIGHTS:
  • ✓Real-time object detection on edge compute hardware for landing zone validation.
  • ✓Custom MAVLink offboard control loops for obstacle avoidance and precision hover.
  • ✓Integrated emergency parachute payload deployment system.
HARDWARE & ELECTRONICS
  • Custom Carbon-Fiber Frame
  • PX4 Flight Controller
  • Companion Single Board Computer
  • Servo Payload Release Mechanism
  • LiPo Telemetry Sensors
SOFTWARE & FIRMWARE
  • PX4 Autopilot
  • ROS2 Humble
  • Python OpenCV
  • YOLOv8 Edge Model
  • MAVSDK
ALGORITHMS & CONTROL LOOPS
  • Autonomous Path Planning (A*)
  • Visual Marker Precision Hover
  • Kalman Filter Sensor Fusion
COMMUNICATION PROTOCOLS
  • MAVLink 2.0
  • UART
  • I2C
  • UDP Telemetry

ENGINEERING CHALLENGES OVERCOME

  • Mitigating electromagnetic interference (EMI) between High-Amp ESC power traces and sensitive GPS/IMU sensors.
  • Maintaining low-latency offboard control during rapid wind gust disturbances.

MY DIRECT CONTRIBUTIONS

  • Designed full mechanical UAV frame, payload drop mechanism, and power distribution PCB.
  • Programmed companion computer offboard control scripts in Python using ROS2 and MAVLink.
  • Tested and validated field flight performance in multi-rotor hover and payload delivery modes.

VALIDATED SYSTEM RESULTS

  • ▸Achieved autonomous landing marker detection and precise delivery release within tight margin tolerances.

KEY ENGINEERING LESSONS LEARNED

  • ▸Isolating power distribution from signal buses is imperative for reliable GPS locking in high-current aerospace platforms.

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