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02 / Autonomy / Research hardware

UAV/UGV Gas-Sensing Platform

UAV and ground-robot platforms supporting autonomous gas-source localization and environmental sensing research.

Status
In development
My role
UAV co-design & system integration
Context
MESA Lab / Collaborative research
Tools & methods
UAV Design · Gas Sensing · ROS
Assembled multirotor UAV with commercial frame, propulsion components, landing gear, and wiring in the lab
FIG. 00 Co-designed UAV platform assembled for continued integration. Flight testing has not yet occurred. View full size ↗

I co-designed the UAV with another team member, including component selection, thrust and power sizing, and integration planning for future source-localization experiments. The platform is being developed alongside a ground robot and simulation workflow.

PROJECT CONTEXT

Project origin

The UAV originated during planning for E2E-Methane-IQ, a proposed multi-scale methane-mapping effort combining satellite, aerial, and ground sensing across the western United States. UC Merced's proposed role focused on high-resolution sensing in the San Joaquin Valley.

The broader program did not proceed after funding was cut. UAV design work continued, and the platform is now being repurposed for autonomous gas-source localization research.

UAV CO-DESIGN / INTEGRATION

My work

  • Co-designed the UAV configuration with another team member.
  • Developed thrust-to-weight and power-sizing calculations, and evaluated payload and endurance requirements.
  • Supported motor, propeller, ESC, and battery selection.
  • Contributed to limited custom fabrication, including motor mounts.
  • Assisted with early ROS-based UAV/UGV coordination and portions of the Isaac Sim workflow.
  • Contributed to the broader research effort and co-authored the related paper.

HARDWARE / SIZING / INTEGRATION

Developing the platforms

AERIAL PLATFORM

Designing the aerial platform

The UAV was developed through system-level component selection and sizing, with most hardware assembled from commercial components. I evaluated propulsion, batteries, frame requirements, payload capacity, and electrical demand as an integrated system alongside my co-designer.

Propulsion margin

Thrust-to-weight calculations informed motor, propeller, and electronic speed controller selection.

Power & endurance

Current draw, power distribution, battery capacity, and estimated flight endurance were considered together.

Payload & integration

Payload allowance and integration margin guided the configuration. Custom fabrication was limited, including motor mounts.

PHYSICAL INTEGRATION

From design to hardware

Long component lead times delayed physical integration. The major hardware has now arrived, and the platform has been assembled for continued development.

Current work focuses on hardware verification, integration, and preparation for controlled testing. Flight performance and physical gas-source localization have not yet been validated.

UAV on a laboratory table with its upper cover removed, exposing electronics and wiring
FIG. 01 UAV hardware during integration, with onboard components accessible for verification. View full size ↗

GROUND PLATFORM

Ground-robot integration

A pre-existing omnidirectional ground robot from another project is being repurposed as the terrestrial half of the sensing system. I did not design or build this UGV.

Its intended role is close-range localization and follow-up measurements, complementing the UAV's planned wider-area search capability.

Pre-existing ground robot with omnidirectional wheels, onboard electronics, and sensing hardware
FIG. 02 Pre-existing UGV platform being repurposed for coordinated gas-source localization experiments. View full size ↗

ROS / INTENDED WORKFLOW

Multi-platform coordination

I contributed to early ROS-based coordination work between the UAV and UGV. The intended workflow uses aerial sensing to identify promising search regions, followed by closer-range ground localization and measurements.

Aerial

Wide-area sensing and search-region identification.

Ground

Close-range localization and follow-up measurements.

This describes the planned architecture. A coordinated aerial-to-ground sensing mission has not yet been demonstrated physically.

SUPPORTING SIMULATION WORK

Simulation and control prototyping

Simulation was used to explore ground-platform control and integration before physical experiments. I assisted with portions of the Isaac Sim setup and control workflow; the majority of this simulation development was led by another team member.

NVIDIA Isaac Sim workspace showing a simulated ground robot, connected action-graph nodes, and controller properties
FIG. 03 NVIDIA Isaac Sim environment used for early differential-drive and control-logic development. View full size ↗

SYSTEMS ENGINEERING

From sensing algorithm to physical platform

The long-term challenge is connecting localization methods to sensing platforms that can operate in real environments. The UAV, UGV, simulation environment, ROS coordination, and localization framework each contribute a different layer.

My work centered on the physical aerial platform and supporting integration, helping prepare the hardware/software foundation for future testing.

RELATED RESEARCH

Gas-source localization

The broader research investigates how an sUAS can navigate turbulent concentration fields and locate an unknown gas source using information-guided planning, reinforcement learning, and safety constraints.

The source-localization and reinforcement-learning framework was primarily developed by Sachin and other research-team members. My contributions focused on UAV co-design, system integration, and supporting hardware/software work.

RELATED PUBLICATION / 2026

Information-Guided Safe Reinforcement Learning for Autonomous Gas Source Localization using sUAS

Sachin Giri, Thomas Zhao, Matthew Huynh, YangQuan Chen

View paper ↗

PHYSICAL HARDWARE

Current status

The UAV is assembled after extended component lead times, and the project is preparing for flight and gas-sensing experiments. The ground platform is being adapted for the same research effort.

Physical testing is planned. The UAV has not yet undergone flight testing, and end-to-end gas-source localization has not been demonstrated in hardware.

SIMULATION TO VALIDATION

Preparing for physical validation

Localization methods, safety logic, and platform-control workflows continue to be developed in simulation. These research and simulation activities are distinct from validation of the assembled hardware.

The next work connects hardware verification, sensing integration, and controlled physical experiments.