Pregled bibliografske jedinice broj: 821698
Singularity-Free Time Integration of Rotational Quaternions Using Non-Redundant Ordinary Differential Equations
Singularity-Free Time Integration of Rotational Quaternions Using Non-Redundant Ordinary Differential Equations // Multibody system dynamics, 38 (2016), 3; 201-225 doi:10.1007/s11044-016-9518-7 (međunarodna recenzija, članak, znanstveni)
CROSBI ID: 821698 Za ispravke kontaktirajte CROSBI podršku putem web obrasca
Naslov
Singularity-Free Time Integration of Rotational Quaternions Using Non-Redundant Ordinary Differential Equations
Autori
Terze, Zdravko ; Mueller, Andreas ; Zlatar, Dario
Izvornik
Multibody system dynamics (1384-5640) 38
(2016), 3;
201-225
Vrsta, podvrsta i kategorija rada
Radovi u časopisima, članak, znanstveni
Ključne riječi
Time integration schemes ; Spatial rotations ; Rotational quaternions ; Integration of quaternions ; Lie groups ; Special orthogonal group SO(3) ; Symplectic group Sp(1) ; Special unitary group SU(2)
Sažetak
A novel ODE time stepping scheme for solving rotational kinematics in terms of unit quaternions is presented in the paper. This scheme inherently respects the unit-length condition without including it explicitly as a constraint equation, as it is common practice. In the standard algorithms, the unit-length condition is included as an additional equation leading to kinematical equations in the form of a system of differential-algebraic equations (DAEs). On the contrary, the proposed method is based on numerical integration of the kinematic relations in terms of the instantaneous rotation vector that form a system of ordinary differential equations (ODEs) on the Lie algebra so(3) of the rotation group SO(3). This rotation vector defines an incremental rotation (and thus the associated incremental unit quaternion), and the rotation update is determined by the exponential mapping on the quaternion group. Since the kinematic ODE on so(3) can be solved by using any standard (possibly higher-order) ODE integration scheme, the proposed method yields a non-redundant integration algorithm for the rotational kinematics in terms of unit quaternions, avoiding integration of DAE equations. Besides being ‘more elegant’—in the opinion of the authors—this integration procedure also exhibits numerical advantages in terms of better accuracy when longer integration steps are applied during simulation. As presented in the paper, the numerical integration of three non-linear ODEs in terms of the rotation vector as canonical coordinates achieves a higher accuracy compared to integrating the four (linear in ODE part) standard-quaternion DAE system. In summary, this paper solves the long-standing problem of the necessity of imposing the unit-length constraint equation during integration of quaternions, i.e. the need to deal with DAE’s in the context of such kinematical model, which has been a major drawback of using quaternions, and a numerical scheme is presented that also allows for longer integration steps during kinematic reconstruction of large three-dimensional rotations.
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
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
Uključenost u ostale bibliografske baze podataka::
- INSPEC
- Zentrallblatt für Mathematik/Mathematical Abstracts
- Science Citation Index, Science Citation Index Expanded, Journal Citation Reports, SCOPUS, Google Scholar, EBSCO, Academic OneFile, CSA Environmental Sciences, Computing and Technology, EI-Compendex, Gale, INIS Atomindex, MathEDUC, Mathematical Reviews, OCLC, Referativnyi Zhurnal (VINITI), SCImago, STMA-Z, Summon by ProQuest