Pregled bibliografske jedinice broj: 657118
Dynamic Simulation of Helicopter Airborne Maneuvers with Numerical Integration Scheme in Lie-Group Setting
Dynamic Simulation of Helicopter Airborne Maneuvers with Numerical Integration Scheme in Lie-Group Setting // ECCOMAS Thematic Conference Multibody Dynamics 2013 Book of Abstracts / Terze, Zdravko (ur.).
Zagreb: Fakultet strojarstva i brodogradnje Sveučilišta u Zagrebu, 2013. str. 25-26 (predavanje, međunarodna recenzija, sažetak, znanstveni)
CROSBI ID: 657118 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
Dynamic Simulation of Helicopter Airborne Maneuvers with Numerical Integration Scheme in Lie-Group Setting
Autori
Terze, Zdravko ; Vrdoljak, Milan ; Zlatar, Dario
Vrsta, podvrsta i kategorija rada
Sažeci sa skupova, sažetak, znanstveni
Izvornik
ECCOMAS Thematic Conference Multibody Dynamics 2013 Book of Abstracts
/ Terze, Zdravko - Zagreb : Fakultet strojarstva i brodogradnje Sveučilišta u Zagrebu, 2013, 25-26
ISBN
978-953-7738-21-1
Skup
Multibody Dynamics 2013, An ECCOMAS Thematic Conference
Mjesto i datum
Zagreb, Hrvatska, 01.07.2013. - 04.07.2013
Vrsta sudjelovanja
Predavanje
Vrsta recenzije
Međunarodna recenzija
Ključne riječi
Lie-groups; Numerical Integration Methods; DAE systems; Helicopter Maneuvers; Inverse Dynamics Control Problem
Sažetak
Dynamic simulation procedures of the aircraft 3D motion need robust and efficient integration methods in order to allow for reliable (and possibly real-time) simulation missions. Derivation of such integration schemes in coordinate-free Liegroup settings is especially efficient since Lie-group dynamical models operate directly on SO(3) rotational matrices and angular velocities, avoiding local rotation parameters and artificial algebraic constraints as well as kinematical differential equations. These integration features of the coordinate-free formulations should be especially beneficial for the flight vehicle simulation missions since a realization of the aircraft complex 3D maneuvers often requires numerical forward dynamics that includes complete 3D rotation domain. In such cases, the utilization of the ‘standard’ vector-space-based modeling procedures (with the local rotation parameters) leads toward kinematical singularities and re-parameterization of the rotation domain, which requires further computational burden. Along this line, a numerical integration scheme in Lie-group settings for the helicopter forward dynamics as well as inverse dynamics control problem is presented and discussed in the paper.
Izvorni jezik
Engleski
Znanstvena područja
Matematika, Strojarstvo, Zrakoplovstvo, raketna i svemirska tehnika
POVEZANOST RADA
Projekti:
120-1201829-1664 - Numeričke simulacijske procedure dinamike slijetanja elastičnog zrakoplova (Terze, Zdravko, MZOS ) ( CroRIS)
Ustanove:
Fakultet strojarstva i brodogradnje, Zagreb