Pregled bibliografske jedinice broj: 1173160
Optimization of flapping wing dynamics for Martian atmosphere via DMOC approach
Optimization of flapping wing dynamics for Martian atmosphere via DMOC approach // ECCOMAS Thematic Conference on Multibody Dynamics
Budimpešta, Mađarska, 2021. str. 310-311 (predavanje, međunarodna recenzija, prošireni sažetak, znanstveni)
CROSBI ID: 1173160 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
Optimization of flapping wing dynamics for Martian
atmosphere via DMOC approach
Autori
Terze, Zdravko ; Pandža, Viktor ; Kasalo, Marko ; Zlatar, Dario
Vrsta, podvrsta i kategorija rada
Sažeci sa skupova, prošireni sažetak, znanstveni
Skup
ECCOMAS Thematic Conference on Multibody Dynamics
Mjesto i datum
Budimpešta, Mađarska, 12.12.2021. - 15.12.2021
Vrsta sudjelovanja
Predavanje
Vrsta recenzije
Međunarodna recenzija
Ključne riječi
Flapping-wing ; Discrete mechanics and optimal control ; Optimization
Sažetak
NASA's Ingenuity Mars Helicopter has recently performed the first powered controlled flight on another planet. However, in spite of success of this mission, rotary wing solution might not be the optimal technology for flying in thin Martian atmosphere. The low density of the atmosphere (only 1% of the Earth's) forces the aircraft to fly at low Re numbers, which significantly deteriorates the performance of a rotary wing. On the other hand, insects fly very efficiently at the same Reynolds numbers, with great aerial capabilities, which makes the insect-type aircraft a promising concept for Mars exploration. To this end, the novel optimization algorithm for development of insect-type aerial vehicle, capable of flight in Martian atmosphere, is proposed. The optimization algorithm combines Discrete Mechanics and Optimal Control (DMOC) approach with quasi- steady aerodynamical model. Results of the numerical experiment indicate that the developed optimization algorithm can be successfully used for computationally efficient optimization of design and dynamics of an insect-type flapping aerial vehicle for Mars exploration purposes — where higher fidelity fluid-structure coupled procedures fail to deliver because of computational non-efficiency. The next natural step, in the development process of the presented algorithm and research of flapping flight on Mars, is to expand the existing aerodynamic model with forward flight features.
Izvorni jezik
Engleski
Znanstvena područja
Zrakoplovstvo, raketna i svemirska tehnika
POVEZANOST RADA
Projekti:
IP-2016-06-6696 - NUMERIČKI EFIKASNI RAČUNALNI ALGORITMI ZA UGRADBENE MULTI-FIZIKALNE SUSTAVE U VEKTORSKIM PROSTORIMA I NA MNOGOSTRUKOSTIMA (NUMECA4EMBEDDED) (Terze, Zdravko, HRZZ - 2016-06) ( CroRIS)
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Ustanove:
Fakultet strojarstva i brodogradnje, Zagreb