Pregled bibliografske jedinice broj: 1115210
Total Energy-Based Approach in VX-3 UAV Flight Dynamics Analysis
Total Energy-Based Approach in VX-3 UAV Flight Dynamics Analysis // 2020 5th International Conference on Smart and Sustainable Technologies (SpliTech) - proceedings
online: Institute of Electrical and Electronics Engineers (IEEE), 2020. str. 1-5 doi:10.23919/SpliTech49282.2020.9243850 (poster, međunarodna recenzija, sažetak, znanstveni)
CROSBI ID: 1115210 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
Total Energy-Based Approach in VX-3 UAV Flight
Dynamics Analysis
Autori
Vuković, Danijel ; Andoga, Rudolf ; Gašparović, Goran ; Kelemen, Miroslav
Vrsta, podvrsta i kategorija rada
Sažeci sa skupova, sažetak, znanstveni
Izvornik
2020 5th International Conference on Smart and Sustainable Technologies (SpliTech) - proceedings
/ - : Institute of Electrical and Electronics Engineers (IEEE), 2020, 1-5
Skup
5th International Conference on Smart and Sustainable Technologies (SpliTech 2020)
Mjesto i datum
Online, 23.09.2020. - 26.09.2020
Vrsta sudjelovanja
Poster
Vrsta recenzije
Međunarodna recenzija
Ključne riječi
potential energy ; control systems ; numerical simulation ; numerical models ; aircraft ; vehicle dynamics ; aerospace control
Sažetak
By the term of flight dynamics, we refer to the general study of performance, stability and control particularly for VX- 3 Unmanned Aerial Vehicle (UAV) during the flight. Each of these aspects of aircraft flight is described separately through the defined flight regime conditions and considering the specific aircraft configuration and geometry aspects. The calculation of an individual flight mode involves the analysis and definition of kinematic and dynamic parameters that are entered into the equations of motion derived from 2nd Newton's Law. The result of the calculated performance is shown in the diagram of the dependence of height and speed (H-V diagram) with a parametric representation of other quantities of interest. Performance diagram show the envelope, i.e. the operating area of an aircraft with optimal modes of interest and maximum operational limitations (e.g. maximum altitude or flight ceiling).
Izvorni jezik
Engleski
Znanstvena područja
Računarstvo, Strojarstvo, Zrakoplovstvo, raketna i svemirska tehnika
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