Pregled bibliografske jedinice broj: 1112089
Optimized flapping wing dynamics via DMOC approach
Optimized flapping wing dynamics via DMOC approach // Nonlinear Dynamics, 103 (2021), 1; 399-417 doi:10.1007/s11071-020-06119-y (međunarodna recenzija, članak, znanstveni)
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Naslov
Optimized flapping wing dynamics via DMOC approach
Autori
Terze, Zdravko ; Pandža, Viktor ; Kasalo, Marko ; Zlatar, Dario
Izvornik
Nonlinear Dynamics (0924-090X) 103
(2021), 1;
399-417
Vrsta, podvrsta i kategorija rada
Radovi u časopisima, članak, znanstveni
Ključne riječi
Flapping wing ; Discrete mechanics and optimal control ; Optimization
Sažetak
Outstanding aerial capabilities that insects present in nature inspire researchers to undertake a challenge to develop a flapping aerial vehicle with performances unmatched by any manmade object. However, the complex aerodynamic phenomena crucial for the insect flight are not easily understood, let alone modeled and utilized for flight. The researchers managed to develop a quasi-steady aerodynamic model capable of capturing the most important aspects of a fruit fly-like insect flight, while still being efficient enough to allow for the usage in the flapping mechanism optimization loop. This experimentally justified quasi-steady model is used in the paper as a building block for creating a novel optimization algorithm, based on the discrete mechanics and optimal control framework. When compared to the conventional approaches to design optimization, this framework includes the natural description of the energy cost function, while incorporating the physical laws in the form of a discrete Lagrange–d’ Alembert equations inherently in optimization constraints. This leads to the discrete description of the inherently continuous problem, allowing the algorithm to search for the optimal solutions in the whole domain. In other words, in contrast to the conventional approaches involving the assumption on the function family and subsequent optimization on the parameters of that function type, this approach is not constrained by the user input and is capable of yielding any solution that respects the physical laws. As presented by the numerical test cases, optimizing the flapping patterns of a fruit fly-like aerial vehicle in standstill hovering leads to both effective and robust optimization tool.
Izvorni jezik
Engleski
Znanstvena područja
Strojarstvo, Zrakoplovstvo, raketna i svemirska tehnika
POVEZANOST RADA
Ustanove:
Fakultet strojarstva i brodogradnje, Zagreb
Citiraj ovu publikaciju:
Časopis indeksira:
- Current Contents Connect (CCC)
- Web of Science Core Collection (WoSCC)
- Science Citation Index Expanded (SCI-EXP)
- SCI-EXP, SSCI i/ili A&HCI
- Scopus