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Yogesh E S

Aeronautical & Autonomy Systems Engineer
yogeshes376@gmail.com 📞 +91 78926 34405 📍 Bengaluru, India 🔗 LinkedIn 🔗 Portfolio 🔗 GitHub
🏆 120+ BVLOS Sorties 🏆 25% Vibration Reduction 🏆 40% Network Overhead Cut 🏆 ±1.2 m Position Hold 🏆 33% GCS Setup Reduction

Professional Summary

Aeronautical & UAV Systems Engineer with end-to-end ownership of autonomous drone development from bare-metal ESP32-S3 autopilot PCB design and ArduPilot HAL integration to ROS 2 swarm middleware and BVLOS field operations. Designed, built, and flight-tested custom flight controllers with EKF3 sensor fusion; commanded operations across a 20+ airframe fleet through 120+ sorties under DGCA UAS Rules 2021. Seeking to bring this depth across the full stack from sensor integration to autonomous mission execution at a company building mission-critical UAV systems.

Core Competencies

Flight Software & Autopilot
ArduPilot (HAL Porting/Integration) PX4 Autopilot MAVLink v2 SITL / HIL Test Environments Autopilot Failsafe Design Flight Log Diagnostics
Robotics & Middleware
ROS 2 (Humble/Jazzy) rclcpp tf2 nav2 Zenoh DDS Micro-XRCE-DDS Behavior Trees Gazebo Harmonic RViz2
Embedded & Avionics Hardware
Custom Autopilot PCB Design (ESP32-S3) FreeRTOS DSHOT/ESC Wiring Sensor Bring-Up (SPI, I2C, CAN, UART) Companion Computer Integration
GNC & Autonomy
EKF3 Sensor Fusion Offboard Path Planning (A*) Waypoint Navigation Swarm Coordination GPS-Denied IR Triangulation Geofencing
Software, Tools & Analysis
Python C++ PyTorch TensorFlow Lite Micro OpenVSP OpenFOAM CFD PrePoMax/CalculiX FEA QGroundControl Mission Planner
Regulations & Operations
DGCA UAS Rules 2021 BVLOS Operations Ground Control Station (GCS) Management Flight Test Planning SOPs & Safety Protocols

Professional Experience

UAV Systems Engineer

Novatech Robo Pvt. Ltd.
📍 Bengaluru, India 📅 Jun 2024 — Present
  • Commanded BVLOS flight test operations across a 20+ airframe fleet logging 120+ sorties with zero incidents executing pre-flight airworthiness checks, real-time telemetry monitoring, and structured post-flight debrief cycles in compliance with DGCA UAS Rules 2021.
  • Authored corporate SOPs for a 5-pilot crew, standardizing pre-flight checklists, emergency response protocols, GCS configuration procedures, and bench-test validation logic; adopted as the baseline operating framework for all new airframe integrations.
  • Built a Python telemetry diagnostic pipeline to parse ArduPilot .bin logs for IMU vibration peaks and EKF3 residuals; applied FFT-driven motor-mount isolation across 5 platforms, reducing structural vibration levels by 25% and extending drivetrain service intervals.
  • Integrated custom ESP32-S3 autopilots with DSHOT ESC wiring and payload cameras; configured offboard ROS 2 (rclcpp) autonomous waypoint-sequencing and geofencing fail-safe behaviors, cutting pre-mission GCS setup time from ~45 min to ~30 min per sortie (33% reduction).
  • Executed real-time GCS PID loop tuning to eliminate roll/pitch transients and optimize battery draw across multiple airframe configurations; delivered hands-on drone assembly and calibration workshops to 120+ engineers across 6 cohort groups.

NDT & Inspection Engineer (Intern)

Trinity NDT Engineers
📍 Bengaluru, India 📅 Feb 2023 — May 2023
  • Performed Radiographic Testing (RT), UT, and Positive Material Identification (PMI) on 150+ aerospace propulsion components for GTRE (DRDO), ensuring airworthiness compliance and authoring inspection reports to AS/NAS quality standards.

Project Experience

AeroCore-S3 - Bare-Metal Custom Flight Controller

ESP32-S3 ArduPilot HAL SPI / I2C Bus EKF3 Fusion PCB Design

Architected a full custom flight controller from schematic to airborne hardware: designed SPI bus topology for BMI270 IMU and BMP581 barometer at sub-10 MHz, resolving clock jitter and bus contention during firmware bringup. Wrote custom HAL interface mappings in ArduPilot for high-speed SPI sensor communication; validated EKF3 sensor fusion through a structured flight test matrix static hover (±1.2 m position hold), GPS-assisted loiter, and full autonomous waypoint execution confirming stable attitude estimation across all envelopes. Published complete flight logs, PCB schematics, and flight footage at github.com/yogesh031020/AeroCore-S3.

Project TRINITY - Decentralized Swarm Coordination Engine

C++ ROS 2 Humble Zenoh DDS Raspberry Pi 4 Gazebo Harmonic

Developed a C++ boids algorithm swarm coordination library running inside isolated ROS 2 namespaces, enabling decentralized multi-agent path planning without a central broker or single point of failure. Integrated Eclipse Zenoh router for peer to peer telemetry synchronization, cutting active network overhead by 40% versus pure ROS 2 DDS validated by bandwidth and RTT profiling on Raspberry Pi 4 companion computers. Visualized real-time swarm state and collision avoidance boundaries in RViz2; full system validated in Gazebo Harmonic SITL before hardware integration.

Autonomous Warehouse Quadcopter v2 - GPS-Denied Autonomy

ESP32-S3 FreeRTOS Kernel IR Triangulation MAVLink telemetry TFLite Micro

Deployed a dual-core FreeRTOS architecture on an ESP32-S3 companion computer: Core 0 handling A* pathfinding and IR triangulation; Core 1 managing MAVLink telemetry and ultrasonic obstacle avoidance achieving <40 ms full control loop latency. Implemented a 4-beacon TSOP38238 IR sensor array for dynamic spatial triangulation, achieving ±3cm docking precision for automated payload pickup in GPS-denied warehouse environments. Deployed a TensorFlow Lite Micro model onboard for human-obstacle classification, triggering MG90S servo safe-release failsafes on detection.

Project ICARUS - HALE Airframe Design & CFD/FEA Optimization

OpenVSP OpenFOAM CFD PrePoMax FEA CalculiX PyTorch ML

Executed a closed-loop design iteration on a 3.0m High-Altitude Long-Endurance (HALE) UAV: aerodynamic shaping in OpenVSP, structural boundary certification in PrePoMax/CalculiX FEA, and low-speed regime validation via OpenFOAM CFD. Trained a PyTorch surrogate model on drag-weight trade surfaces across aspect ratio and spar geometry sweeps, achieving an 11.9% lift efficiency gain over the baseline all design decisions data-driven from CFD and FEA outputs.

Education

B.E. in Aeronautical Engineering

SJC Institute of Technology (VTU)
📍 Chikkaballapura, India 📅 2019 — 2023

Final Year Project: Prototype Design & Analysis of a Valveless Pulsejet Engine - propulsion systems, combustion analysis, structural testing

Training Focus

Professional Non-Destructive Testing (NDT) Level II Certification (UT, PT, RT) | Trinity NDT Engineers

Languages

English (Professional) • Hindi • Kannada • Tamil