Lightweight aircraft design: Integrating biomechanics and algorithm optimization for drone construction using paper materials
Abstract
Lightweight aircraft design emphasizes materials like composites, alloys, and advanced polymers to reduce weight while ensuring structural integrity. Streamlined aerodynamics, efficient propulsion systems, and optimized component layout further enhance performance. The purpose of this research is to develop an innovative aircraft design model for drones, integrating algorithm optimization techniques and lightweight materials to enhance the performance and efficiency of drones with the utilization of open-source software. We apply this structure to the construction of drones with fixed-wing (FW) and vertical take-off and landing (VTOL) configurations. The aircraft’s body is constructed using lightweight materials such as glass fiber fabric (Gff) and extruded polystyrene foam (XPS), employing a vacuum-assisted wet layup technique for fabrication. Multi-objective Co-evolving Ant Colony Optimization (MC-ACO) was used to improve the construction of drones with VTOL and FW capabilities. This strategy enabled it to be easier to achieve the trade-offs required for a generalist drone design, such as range, payload capabilities, and swarm operations, which were then evaluated against commercially available software to evaluate the effectiveness. Incorporating biomechanics into the design method permits higher consideration of user interaction with drones. The findings indicate that low-fidelity architecture is a suitable starting point for prototyping under limited time frames. The paper concludes with a discussion of the technical constraints of employing free software, as well as some practical concerns for flight testing drones with hybrid configurations.
References
1. Hildmann H, Kovacs E. Review: Using Unmanned Aerial Vehicles (UAVs) as Mobile Sensing Platforms (MSPs) for Disaster Response, Civil Security and Public Safety. Drones. 2019; 3(3): 59. doi: 10.3390/drones3030059
2. Emimi M, Khaleel M, Alkrash A. The Current Opportunities and Challenges in Drone Technology. Int. J. Electr. Eng. And Sustain. 2023; 1(3): 74-89.
3. Dams B, Sareh S, Zhang K, et al. Remote three-dimensional printing of polymer structures using drones. Proceedings of the Institution of Civil Engineers - Construction Materials. 2017; 1-31. doi: 10.1680/jcoma.17.00013
4. Rajak D, Pagar D, Menezes P, et al. Fiber-Reinforced Polymer Composites: Manufacturing, Properties, and Applications. Polymers. 2019; 11(10): 1667. doi: 10.3390/polym11101667
5. Sun J, Cai F, Tao D, et al. Enhanced Thermal Insulation of the Hollow Glass Microsphere/Glass Fiber Fabric Textile Composite Material. Polymers. 2021; 13(4): 505. doi: 10.3390/polym13040505
6. Zhu H, Nie H, Zhang L, et al. Design and assessment of octocopter drones with improved aerodynamic efficiency and performance. Aerospace Science and Technology. 2020; 106: 106206. doi: 10.1016/j.ast.2020.106206
7. Chen Z, Zhang Z, Xie J, et al. Metaheuristic optimization method for compact reactor radiation shielding design based on genetic algorithm. Annals of Nuclear Energy. 2019; 134: 318-329. doi: 10.1016/j.anucene.2019.06.031
8. Osaba E, Villar-Rodriguez E, Del Ser J, et al. A Tutorial On the design, experimentation and application of metaheuristic algorithms to real-World optimization problems. Swarm and Evolutionary Computation. 2021; 64: 100888. doi: 10.1016/j.swevo.2021.100888
9. Badini S, Regondi S, Pugliese R. Unleashing the Power of Artificial Intelligence in Materials Design. Materials. 2023; 16(17): 5927. doi: 10.3390/ma16175927
10. Cañas JM, Martín-Martín D, Arias P, et al. Open-Source Drone Programming Course for Distance Engineering Education. Electronics. 2020; 9(12): 2163. doi: 10.3390/electronics9122163
11. Kopar M, Yıldız AR, Yıldız BS. Optimum design of a composite drone component using slime mold algorithm. Materials Testing. 2023; 65(12): 1857-1864. doi: 10.1515/mt-2023-0245
12. Skarka W, Jałowiecki A. Automation of a Thin-Layer Load-Bearing Structure Design on the Example of High Altitude Long Endurance Unmanned Aerial Vehicle (HALE UAV). Applied Sciences. 2021; 11(6): 2645. doi: 10.3390/app11062645
13. Pecho P, Ažaltovič V, Kandera B, et al. Introduction study of design and layout of UAVs 3D printed wings in relation to optimal lightweight and load distribution. Transportation Research Procedia. 2019; 40: 861-868. doi: 10.1016/j.trpro.2019.07.121
14. Yilmaz F, Şahin M, Gürses E. Weight reduction of an unmanned aerial vehicle pylon fitting by topology optimization and additive manufacturing with electron beam melting. Journal of Additive Manufacturing Technologies. 2021; 1(2). doi: 10.18416/JAMTECH.2111553
15. Yap YL, Toh W, Giam A, et al. Topology optimization and 3D printing of micro-drone: Numerical design with experimental testing. International Journal of Mechanical Sciences. 2023; 237: 107771. doi: 10.1016/j.ijmecsci.2022.107771
16. Balayan A, Mallick R, Dwivedi S, et al. Optimal Design of Quadcopter Chassis Using Generative Design and Lightweight Materials to Advance Precision Agriculture. Machines. 2024; 12(3): 187. doi: 10.3390/machines12030187
17. Maricic S, Haber IM, Veljovic I, et al. Implementation of optimum additive technologies design for unmanned aerial vehicle take-off weight increase. Eureka: Physics and Engineering. 2020; (6): 50-60. doi: 10.21303/2461-4262.2020.001514
18. García-Gascón C, Castelló-Pedrero P, García-Manrique JA. Minimal Surfaces as an Innovative Solution for the Design of an Additive Manufactured Solar-Powered Unmanned Aerial Vehicle (UAV). Drones. 2022; 6(10): 285. doi: 10.3390/drones6100285
19. Maity R, Mishra R, Kumar Pattnaik P, et al. Selection of sustainable material for the construction of UAV aerodynamic wing using MCDM technique. Materials Today: Proceedings. doi: 10.1016/j.matpr.2023.12.025
20. Dinovitzer M, Miller C, Hacker A, et al. Structural Development and Multiscale Design Optimization of Additively Manufactured UAV with Blended Wing Body Configuration Employing Lattice Materials. AIAA Scitech 2019 Forum. doi: 10.2514/6.2019-2048
21. Xiao R, Li X, Jia H, et al. 3D printing of dual phase-strengthened microlattices for lightweight micro aerial vehicles. Materials & Design. 2021; 206: 109767. doi: 10.1016/j.matdes.2021.109767
22. Elelwi M, Pinto FS, Botez RM, et al. Multidisciplinary Optimization for Weight Saving in a Variable Tapered Span-Morphing Wing Using Composite Materials—Application to the UAS-S4. Actuators. 2022; 11(5): 121. doi: 10.3390/act11050121
23. Jayakumar SS, Subramaniam IP, Stanislaus Arputharaj B, et al. Design, control, aerodynamic performances, and structural integrity investigations of compact ducted drone with co-axial propeller for high altitude surveillance. Scientific Reports. 2024; 14(1). doi: 10.1038/s41598-024-54174-x
24. Raja V, AL-bonsrulah HAZ, Gnanasekaran RK, et al. Design and advanced computational approaches based comprehensive structural parametric investigations of rotary-wing UAV imposed with conventional and hybrid computational composite materials: A validated investigation. Frontiers in Materials. 2023; 10. doi: 10.3389/fmats.2023.1096839
25. Nvss S, Esakki B, Yang LJ, et al. Design and Development of Unibody Quadcopter Structure Using Optimization and Additive Manufacturing Techniques. Designs. 2022; 6(1): 8. doi: 10.3390/designs6010008
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