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Pregled bibliografske jedinice broj: 657118

Dynamic Simulation of Helicopter Airborne Maneuvers with Numerical Integration Scheme in Lie-Group Setting


Terze, Zdravko; Vrdoljak, Milan; Zlatar, Dario
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)


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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

Profili:

Avatar Url Dario Zlatar (autor)

Avatar Url Milan Vrdoljak (autor)

Avatar Url Zdravko Terze (autor)


Citiraj ovu publikaciju:

Terze, Zdravko; Vrdoljak, Milan; Zlatar, Dario
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)
Terze, Z., Vrdoljak, M. & Zlatar, D. (2013) Dynamic Simulation of Helicopter Airborne Maneuvers with Numerical Integration Scheme in Lie-Group Setting. U: Terze, Z. (ur.)ECCOMAS Thematic Conference Multibody Dynamics 2013 Book of Abstracts.
@article{article, author = {Terze, Zdravko and Vrdoljak, Milan and Zlatar, Dario}, editor = {Terze, Z.}, year = {2013}, pages = {25-26}, keywords = {Lie-groups, Numerical Integration Methods, DAE systems, Helicopter Maneuvers, Inverse Dynamics Control Problem}, isbn = {978-953-7738-21-1}, title = {Dynamic Simulation of Helicopter Airborne Maneuvers with Numerical Integration Scheme in Lie-Group Setting}, keyword = {Lie-groups, Numerical Integration Methods, DAE systems, Helicopter Maneuvers, Inverse Dynamics Control Problem}, publisher = {Fakultet strojarstva i brodogradnje Sveu\v{c}ili\v{s}ta u Zagrebu}, publisherplace = {Zagreb, Hrvatska} }
@article{article, author = {Terze, Zdravko and Vrdoljak, Milan and Zlatar, Dario}, editor = {Terze, Z.}, year = {2013}, pages = {25-26}, keywords = {Lie-groups, Numerical Integration Methods, DAE systems, Helicopter Maneuvers, Inverse Dynamics Control Problem}, isbn = {978-953-7738-21-1}, title = {Dynamic Simulation of Helicopter Airborne Maneuvers with Numerical Integration Scheme in Lie-Group Setting}, keyword = {Lie-groups, Numerical Integration Methods, DAE systems, Helicopter Maneuvers, Inverse Dynamics Control Problem}, publisher = {Fakultet strojarstva i brodogradnje Sveu\v{c}ili\v{s}ta u Zagrebu}, publisherplace = {Zagreb, Hrvatska} }




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