Pregled bibliografske jedinice broj: 591234
Spincopter Wing Design and Flight Control
Spincopter Wing Design and Flight Control // Journal of intelligent & robotic systems, 70 (2013), 1/4; 165-179 doi:10.1007/s10846-012-9725-2 (međunarodna recenzija, članak, znanstveni)
CROSBI ID: 591234 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
Spincopter Wing Design and Flight Control
Autori
Orsag, Matko ; Ćesić, Josip ; Haus, Tomislav ; Bogdan, Stjepan
Izvornik
Journal of intelligent & robotic systems (0921-0296) 70
(2013), 1/4;
165-179
Vrsta, podvrsta i kategorija rada
Radovi u časopisima, članak, znanstveni
Ključne riječi
UAV; rotorcraft; control; aerodynamics
Sažetak
This paper presents dynamical properties of an unmanned aerial vehicle (UAV), called spincopter. The vehicle structure is based on two wings that are forced in rotation (spinning) by propulsion system formed of two propellers. Based on devised dynamical model, that reveals inherent stability of the vehicle, composition of control algorithms for vertical and horizontal movement is proposed. Due to the specific configuration of the propulsion system, movement in horizontal direction is produced by pulsations in rotational speed of propulsion motors. An analysis of influence that such a configuration has on the vehicle dynamics is given. Finally, design recommendations for rotational wings are elaborated, based on extensive simulations of spincopter by using X-Plane® software package.
Izvorni jezik
Engleski
Znanstvena područja
Elektrotehnika
POVEZANOST RADA
Projekti:
036-0363078-3016 - Planiranje i izvođenje zadataka u robotskim i autonomnim sustavima (Bogdan, Stjepan, MZO ) ( CroRIS)
Ustanove:
Fakultet elektrotehnike i računarstva, 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
