Sep 2026· Advances in Science and Technology· Vol 182, pp. 331 - 342· 0 citations· 22 references
Abstract
This paper presents a methodology for the multi-objective optimization of protective structures for DJI Avata 2 unmanned aerial vehicles (UAVs). The modified platforms are specifically adapted for search and rescue (SAR) operations, the inspection of destroyed buildings, infrastructure, and linear facilities, as well as navigation through dense technogenic debris resulting from the martial law conditions in Ukraine. Based on numerical simulation results (FEA and CFD) and the introduction of an integral modification efficiency coefficient (E) that accounts for structural survivability, a rational balance is established between the collision energy-absorption capacity of the exoskeleton and the aerodynamic degradation of thrust. The study demonstrates that the application of optimized hybrid exoskeletons improves the UAV's critical resistance to dynamic impacts by 20–25% while maintaining maneuvering stability in confined spaces. The findings hold practical significance for enhancing the operational reliability of UAVs executing specialized missions in complex and hazardous environments.
Unmanned aerial vehicles (UAVs) have become an indispensable tool for solving a wide range of complex tasks. To improve and increase the efficiency of unmanned aerial vehicles, it is important to optimize their structural elements. Reducing weight and strategically distributing loads while maintaining structural streng...
Nazarii Muliak, O. Stankevych· Computer Systems and Informa...· 0 citations
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.· Международный научный журнал...· 0 citations
This multidisciplinary approach seeks to determine how to upgrade a civilian helicopter to a weapons-capable design by optimizing both integrated aero-structural and mission parameters. The finite element analysis (FEA), computational fluid dynamics (CFD) and key parameters to assess the integrity of components (struc...
D. Kumaresan, R. Asokan, C. J. Babu et al.· Defence Science Journal· 0 citations
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.· Drones· 0 citations
Atmospheric icing is one of the most critical meteorological hazards for unmanned aerial vehicles (UAV), whose operation under adverse conditions—high latitudes, elevated altitudes, long-endurance missions without pilot intervention—particularly exposes them to ice accumulation on aerodynamic surfaces and propellers. U...
R. Avella, C. A. Gonzalez, Paula N. López· Drones· 0 citations
Aiming at the problems of high sea condition susceptibility, low automation level, and high operational risks in the storage, transportation, launching, and recovery of shipborne Autonomous Underwater Vehicles (AUVs) under complex marine wind and wave environments, this paper designs an AUV launching and recovery devic...
Jian-Li Wang, Ming-Wang Song, Xuan Qi et al.· Journal of Physics, Conferen...· 0 citations
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