Skip to content
Open access

In-Service Wind Turbine Blade Inspection: A Multi-UAV Architecture Design and Preliminary Validation

2026 · IEEE Access · Vol 14, pp. 142383-142399 · 0 citations · 39 references

Abstract

Wind turbine blade inspections are critical for ensuring structural integrity and minimizing operational downtime. However, existing methods, such as single Unmanned Aerial Vehicle (UAV) inspections, are limited by trade-offs among coverage, resolution, operational constraints, and often require turbine shutdown. This paper presents a multi-UAV inspection architecture design for in-service wind turbine blade inspection. The proposed architecture design provides a scalable framework for multi-UAV-based inspection of wind turbines during operation, enabling data acquisition without halting the turbine. The system distributes tasks across multiple UAVs, enabling simultaneous global observation, close-range surface imaging, and deflection detection. A ground station is introduced to coordinate the system, aggregate multi-view data, and offload computationally intensive processing. By separating global and local perception tasks, the architecture addresses key limitations of single-UAV systems and supports synchronized data acquisition during regular wind turbine operation. The core components of the system are implemented and evaluated using a scaled wind turbine model. Results demonstrate stable, persistent blade identification, reliable deflection estimation during rotation, and a component-level preliminary validation on embedded hardware platforms in terms of computational and energy requirements.

Read PDF

Similar papers

Open access Sep 2026

Development and Feasibility Assessment of a UAV-Mounted Winch System for Vertical Air Sampling and Atmospheric Profiling

Rotary-wing unmanned aerial vehicles (UAVs) are increasingly used for low-altitude atmospheric monitoring, but rotor-induced flow can bias samples taken close to the airframe or near the ground. This paper presents the design and feasibility assessment of a lightweight UAV-mounted winch that lowers an air-sampling pod...

Rafiul Azim Jowarder, Sheryll Jerez · 0 citations
Sep 2026

Design and multi-domain optimisation of a fixed-wing UAV with payload deployment system

The purpose of this study is to design, analyse, fabricate and validate a fixed-wing UAV for stable low-speed flight, payload carriage and controlled in-flight deployment. It aims to achieve aerodynamic efficiency, structural safety, stability and practical manufacturability for short-range logistics, surveillance...

Aditya Sivaraman, A. Ansari, Aqleem Siddiqui et al. · 0 citations
Open access Aug 2026

An Integrated Force Assessment and Disturbance Compensation Framework for Stable UAV-Based Water-Jet Cleaning

Uncrewed aerial vehicles (UAVs) represent a promising alternative for building facade cleaning, improving efficiency while reducing the risks associated with working at height. However, such operations are particularly challenging due to the reaction forces generated by fluid discharge, which can compromise UAV stabili...

Gálata Martínez-Alonso, E. Aldao, F. Veiga-López et al. · 0 citations
Open access Oct 2026

An integrated framework for multidisciplinary design optimization of unmanned aerial vehicles

The growing demand for high-performance Unmanned Aerial Vehicles (UAVs) in civil, commercial, and defense applications has increased the need for advanced engineering methodologies capable of addressing complex and often conflicting design requirements. Conventional sequential design approaches generally optimize indiv...

Turgunbek Alimov, Jonibek Shukurov, Yusuf Ergashev et al. · 0 citations
Oct 2026

Bottom-up computational design of a hybrid tricopter agricultural spray UAV: propeller, nozzle, tank and airframe CFD optimization

This paper aims to develop and validate a hybrid tri-agri-copter (TAC) unmanned aerial vehicle (UAV) for precision agricultural spraying using a bottom-up computational fluid dynamics (CFD)-first design methodology that sequentially evaluates each sub-system before full-vehicle integration. A 2.5 kg payload...

Darshan Kumar Jayaram, Beena Stanislaus Arputharaj, Ramya Maranan et al. · 0 citations

We use cookies to run the site and, with your consent, for analytics and to show ads. See our Cookie Policy.