15 results on '"symplectic reduction"'
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2. Relative equilibria of mechanical systems with rotational symmetry.
- Author
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Arathoon, Philip
- Subjects
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ROTATIONAL symmetry , *STATIC equilibrium (Physics) , *THREE-body problem , *CLASSICAL mechanics - Abstract
We consider the task of classifying relative equilibria for mechanical systems with rotational symmetry. We divide relative equilibria into two natural groups: a generic class which we call normal, and a non-generic abnormal class. The eigenvalues of the locked inertia tensor descend to shape-space and endow it with the geometric structure of a three-web with the property that any normal relative equilibrium occurs as a critical point of the potential restricted to a leaf from the web. To demonstrate the utility of this web structure we show how the spherical three-body problem gives rise to a web of Cayley cubics on the three-sphere, and use this to fully classify the relative equilibria for the case of equal masses. [ABSTRACT FROM AUTHOR]
- Published
- 2024
- Full Text
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3. Multigraded Hilbert series of invariants, covariants, and symplectic quotients for some rank 1 Lie groups.
- Author
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Barringer, Austin, Herbig, Hans-Christian, Herden, Daniel, Khalid, Saad, Seaton, Christopher, and Walker, Lawton
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FINITE groups , *LIE groups , *ALGEBRA , *ALGORITHMS - Abstract
We compute univariate and multigraded Hilbert series of invariants and covariants of representations of the circle and orthogonal group O 2 (R) . The multigradings considered include the maximal grading associated to the decomposition of the representation into irreducibles as well as the bigrading associated to a cotangent-lifted representation, or equivalently, the bigrading associated to the holomorphic and antiholomorphic parts of the real invariants and covariants. This bigrading induces a bigrading on the algebra of on-shell invariants of the symplectic quotient, and the corresponding Hilbert series are computed as well. We also compute the first few Laurent coefficients of the univariate Hilbert series, give sample calculations of the multigraded Laurent coefficients, and give an example to illustrate the extension of these techniques to the semidirect product of the circle by other finite groups. We describe an algorithm to compute each of the associated Hilbert series. Communicated by Ellen Kirkman [ABSTRACT FROM AUTHOR]
- Published
- 2024
- Full Text
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4. Gluing Affine Vortices.
- Author
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Xu, Guang Bo
- Subjects
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GLUE , *GAGING - Abstract
We provide an analytical construction of the gluing map for stable affine vortices over the upper half plane with the Lagrangian boundary condition. This result is a necessary ingredient in studies of the relation between gauged sigma model and nonlinear sigma model, such as the closed or open quantum Kirwan map. [ABSTRACT FROM AUTHOR]
- Published
- 2024
- Full Text
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5. Reductions: precontact versus presymplectic.
- Author
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Grabowska, Katarzyna and Grabowski, Janusz
- Abstract
We show that contact reductions can be described in terms of symplectic reductions in the traditional Marsden–Weinstein–Meyer as well as the constant rank picture. The point is that we view contact structures as particular (homogeneous) symplectic structures. A group action by contactomorphisms is lifted to a Hamiltonian action on the corresponding symplectic manifold, called the symplectic cover of the contact manifold. In contrast to the majority of the literature in the subject, our approach includes general contact structures (not only co-oriented) and changes the traditional view point: contact Hamiltonians and contact moment maps for contactomorphism groups are no longer defined on the contact manifold itself, but on its symplectic cover. Actually, the developed framework for reductions is slightly more general than purely contact, and includes a precontact and presymplectic setting which is based on the observation that there is a one-to-one correspondence between isomorphism classes of precontact manifolds and certain homogeneous presymplectic manifolds. [ABSTRACT FROM AUTHOR]
- Published
- 2023
- Full Text
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6. A Discrete Version for Vortex Loops in 2D Fluids
- Author
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Vizman, Cornelia, Goos, Gerhard, Founding Editor, Hartmanis, Juris, Founding Editor, Bertino, Elisa, Editorial Board Member, Gao, Wen, Editorial Board Member, Steffen, Bernhard, Editorial Board Member, Yung, Moti, Editorial Board Member, Nielsen, Frank, editor, and Barbaresco, Frédéric, editor
- Published
- 2023
- Full Text
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7. Conic reductions for Hamiltonian actions of U(2) and its maximal torus.
- Author
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Paoletti, Roberto
- Abstract
Suppose given a Hamiltonian and holomorphic action of G = U (2) on a compact Kähler manifold M, with nowhere vanishing moment map. Given an integral coadjoint orbit O for G, under transversality assumptions we shall consider two naturally associated 'conic' reductions. One, which will be denoted M ¯ O G , is taken with respect to the action of G and the cone over O ; another, which will be denoted M ¯ ν T , is taken with respect to the action of the standard maximal torus T ⩽ G and the ray R + ı ν along which the cone over O intersects the positive Weyl chamber. These two reductions share a common 'divisor', which may be viewed heuristically as bridging between their structures. This point of view motivates studying the (rather different) ways in which the two reductions relate to the the latter divisor. In this paper we provide some indications in this direction. Furthermore, we give explicit transversality criteria for a large class of such actions in the projective setting, as well as a description of corresponding reductions as weighted projective varieties, depending on combinatorial data associated to the action and the orbit. [ABSTRACT FROM AUTHOR]
- Published
- 2023
- Full Text
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8. Hilbert series of symplectic quotients by the 2-torus.
- Author
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Herbig, Hans-Christian, Herden, Daniel, and Seaton, Christopher
- Abstract
We compute the Hilbert series of the graded algebra of real regular functions on a linear symplectic quotient by the 2-torus as well as the first four coefficients of the Laurent expansion of this Hilbert series at t = 1 . We describe an algorithm to compute the Hilbert series as well as the Laurent coefficients in explicit examples. [ABSTRACT FROM AUTHOR]
- Published
- 2023
- Full Text
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9. Secular Dynamics for Curved Two-Body Problems.
- Author
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Jackman, Connor
- Subjects
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TWO-body problem (Physics) , *SPACES of constant curvature , *ANGLES , *EQUATIONS of motion , *CURVATURE - Abstract
Consider the dynamics of two point masses on a surface of constant curvature subject to an attractive force analogue of Newton's inverse square law, that is under a 'cotangent' potential. When the distance between the bodies is sufficiently small, the reduced equations of motion may be seen as a perturbation of an integrable system. We take suitable action-angle coordinates to average these perturbing terms and describe dynamical effects of the curvature on the motion of the two-bodies. [ABSTRACT FROM AUTHOR]
- Published
- 2023
- Full Text
- View/download PDF
10. Momentum maps and the Kähler property for base spaces of reductive principal bundles.
- Author
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Greb, Daniel and Miebach, Christian
- Abstract
We investigate the complex geometry of total spaces of reductive principal bundles over compact base spaces and establish a close relation between the Kähler property of the base, momentum maps for the action of a maximal compact subgroup on the total space, and the Kähler property of special equivariant compactifications. We provide many examples illustrating that the main result is optimal. [ABSTRACT FROM AUTHOR]
- Published
- 2023
- Full Text
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11. Symplectic reduction along a submanifold.
- Author
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Crooks, Peter and Mayrand, Maxence
- Subjects
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QUANTUM field theory , *ANALYTIC spaces , *ALGEBRAIC varieties , *TOPOLOGICAL fields , *CONCRETE construction , *SYMPLECTIC geometry - Abstract
We introduce the process of symplectic reduction along a submanifold as a uniform approach to taking quotients in symplectic geometry. This construction holds in the categories of smooth manifolds, complex analytic spaces, and complex algebraic varieties, and has an interpretation in terms of derived stacks in shifted symplectic geometry. It also encompasses Marsden–Weinstein–Meyer reduction, Mikami–Weinstein reduction, the pre-images of Poisson transversals under moment maps, symplectic cutting, symplectic implosion, and the Ginzburg–Kazhdan construction of Moore–Tachikawa varieties in topological quantum field theory. A key feature of our construction is a concrete and systematic association of a Hamiltonian $G$ -space $\mathfrak {M}_{G, S}$ to each pair $(G,S)$ , where $G$ is any Lie group and $S\subseteq \mathrm {Lie}(G)^{*}$ is any submanifold satisfying certain non-degeneracy conditions. The spaces $\mathfrak {M}_{G, S}$ satisfy a universal property for symplectic reduction which generalizes that of the universal imploded cross-section. Although these Hamiltonian $G$ -spaces are explicit and natural from a Lie-theoretic perspective, some of them appear to be new. [ABSTRACT FROM AUTHOR]
- Published
- 2022
- Full Text
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12. Geometry of bundle-valued multisymplectic structures with Lie algebroids.
- Author
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Hirota, Yuji and Ikeda, Noriaki
- Subjects
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ALGEBROIDS , *SYMPLECTIC manifolds , *VECTOR bundles , *GEOMETRY , *SET-valued maps , *SYMMETRY - Abstract
We study multisymplectic structures taking values in vector bundles with connections from the viewpoint of the Hamiltonian symmetry. We introduce the notion of bundle-valued n -plectic structures and exhibit some properties of them. In addition, we define bundle-valued homotopy momentum sections for bundle-valued n -plectic manifolds with Lie algebroids to discuss momentum map theories in both cases of quaternionic Kähler manifolds and hyper-Kähler manifolds. Furthermore, we generalize the Marsden-Weinstein-Meyer reduction theorem for symplectic manifolds and construct two kinds of reductions of vector-valued 1-plectic manifolds. [ABSTRACT FROM AUTHOR]
- Published
- 2024
- Full Text
- View/download PDF
13. Reduced coupled flapping wing-fluid computational model with unsteady vortex wake.
- Author
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Terze, Zdravko, Pandža, Viktor, Andrić, Marijan, and Zlatar, Dario
- Abstract
Insect flight research is propelled by their unmatched flight capabilities. However, complex underlying aerodynamic phenomena make computational modeling of insect-type flapping flight a challenging task, limiting our ability in understanding insect flight and producing aerial vehicles exploiting same aerodynamic phenomena. To this end, novel mid-fidelity approach to modeling insect-type flapping vehicles is proposed. The approach is computationally efficient enough to be used within optimal design and optimal control loops, while not requiring experimental data for fitting model parameters, as opposed to widely used quasi-steady aerodynamic models. The proposed algorithm is based on Helmholtz–Hodge decomposition of fluid velocity into curl-free and divergence-free parts. Curl-free flow is used to accurately model added inertia effects (in almost exact manner), while expressing system dynamics by using wing variables only, after employing symplectic reduction of the coupled wing-fluid system at zero level of vorticity (thus reducing out fluid variables in the process). To this end, all terms in the coupled body-fluid system equations of motion are taken into account, including often neglected terms related to the changing nature of the added inertia matrix (opposed to the constant nature of rigid body mass and inertia matrix). On the other hand—in order to model flapping wing system vorticity effects—divergence-free part of the flow is modeled by a wake of point vortices shed from both leading (characteristic for insect flight) and trailing wing edges. The approach is evaluated for a numerical case involving fruit fly hovering, while quasi-steady aerodynamic model is used as benchmark tool with experimentally validated parameters for the selected test case. The results indicate that the proposed approach is capable of mid-fidelity accurate calculation of aerodynamic loads on the insect-type flapping wings. [ABSTRACT FROM AUTHOR]
- Published
- 2022
- Full Text
- View/download PDF
14. Arnold’s conjecture and symplectic reduction
- Author
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Ibort, A., Martínez Ontalba, Celia, Ibort, A., and Martínez Ontalba, Celia
- Abstract
Fortune (1985) proved Arnold's conjecture for complex projective spaces, by exploiting the fact that CPn-1 is a symplectic quotient of C-n. In this paper, we show that Fortune's approach is universal in the sense that it is possible to translate Arnold's conjecture on any closed symplectic manifold (Q,Omega) to a critical point problem with symmetry on loops in R(2n) With its Standard symplectic structure., CICYT, Depto. de Álgebra, Geometría y Topología, Fac. de Ciencias Matemáticas, TRUE, pub
- Published
- 2023
15. Numerički efikasan računalni model male mahokrilne letjelice temeljen na Hamiltonovim geometrijskim redukcijama
- Author
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Pandža, Viktor and Terze, Zdravko
- Subjects
Flapping flight on Mars ,Vrtložni trag ,Fluidni utjecaj dodane inercije ,TECHNICAL SCIENCES. Aviation, Rocket and Space Technology ,udc:629.7(043.3) ,Mahokrilo insektnog tipa ,Insect-type flapping ,Added inertia ,Tehnika i vrste zračnih vozila ,Spregnut sustav dinamike fluida i sustava više tijela ,Vortex wake ,Mahokrilna letjelica ,Air transport engineering ,TEHNIČKE ZNANOSTI. Zrakoplovstvo, raketna i svemirska tehnika ,Mahokrilni let na Marsu ,Symplectic reduction ,Flapping wing aerial vehicle ,Simplekticka redukcija ,Coupled multibody-fluid system - Abstract
Insect flight capabilities provide fascination for humans and fuel aspirations for development and manufacturing of insect-type flapping wing aerial vehicles. However, complex underlying aerodynamic phenomena limit our abilities in understanding insect flight and producing aerial vehicle exploiting same phenomena. To this end, a novel mid-fidelity approach to insect-type flapping vehicles modeling is proposed. Computational model includes Helmholtz-Hodge decompositon of fluid velocity into curl-free and divergence-free parts. Coupled multibody-fluid system equations of motion are derived, including added inertia effects of the environmental fluid and viscous effects arising as an additional aerodynamic load on a multibody system. Curl-free vector field is utilized to accurately model added inertia effects, while expressing coupled system dynamics by using multibody system variables only, after employing symplectic reduction of the coupled multibody-fluid system. On the other hand, unsteady viscous effects included in the divergence-free vector field are modeled by a wake of irrotational point vortices, shed from both leading (important for insect-type flapping flight) and trailing edges of the flapping wing. A proposed computational model is evaluated on two numerical examples involving insect-type flapping flight. The first test case involves standstill hovering of fruit fly in Earth atmospheric environment, propelled by flapping pattern characterized with smooth flapping angle functions. Second test case involves insect-type flapping wing aerial vehicle performing hovering in Mars atmospheric environment, with flapping pattern input in discrete form, resulting from optimization algorithm. It is concluded from results analysis that the proposed computational model exhibited near real time properties with high load prediction accuracy. Let insekata predstavlja inspiraciju za istraživanje u tehničkim i prirodnim znanostima, zbog njihovih izvrsnih performansi letenja, koje se temelje na naglašenom korištenju nestacionarnih ‘fluid-solid’ utjecaja. Mahokrila insektnog tipa omogućuju energetski efikasan let i brze manevre, zadržavajući male dimenzije te predstavljajući letne performanse s kojima se ne mogu usporediti performanse konstruiranih letjelica (tek su nedavno dizajnirane prve letjelice koje u određenoj mjeri oponašaju let insekta). Razlog tomu jest složena nestacionarna aerodinamika karakteristična za let insekata koja se počela razumijevati tek u protekla tri desetljeća. Između ostalog, otkriveno je da insekti koriste vrtlog otpušten s napadnog ruba krila kako bi dodatno povećali uzgon u usporedbi s istim krilom pri istom napadnom kutu u stacionarnom strujanju bez vrtloga. Fokus istraživača u posljednja dva desetljaća usmjeren je na razvoj i izradu mahokrilne letjelice koja bi koristila iste nestacionarne aerodinamičke fenomene karakteristične za let insekata. Složenost nestacionarnih i izrazito nelinearnih aerodinamičkih fenomena otežava zadaću konstruiranja i optimiranja takve letjelice bez odgovarajućih računalnih alata. Zbog visokih frekvencija mahanja i velike amplitude rotacije krila karakterističnih za let insekata računalni modeli spregnutih zadaća temeljeni na metodi konačnih volumena za modeliranje fluida i posebnih (odvojenih) numeričkih rješavača dinamike uronjenog kinematičkog lanca pokazuju neoptimalne performanse i mogućnost pojava računalnih nestabilnosti. Osim toga, računalno vrijeme potrebno za njihovo izvršavanje čini takve pristupe modeliranja neupotrebljivima unutar konstrukcijskih petlji te unutar petlji za optimalno upravljanje. Iz tog razloga javlja se potreba za računalnim modelom mahokrilne letjelice insektnog tipa koji bi omogućio pouzdano modeliranje signifikantnih aerodinamičkih fenomena uz zadržavanje računalne efikasnosti koja omogućuje primjenu unutar konstrukcijskih petlji te unutar petlji optimalnog upravljanja. U tu svrhu spregnuti sustav krilo-fluid promatra se iz perspektive geometrijske mehanike koja omogućava redukcije spregnutog modela na zajedničkoj mognostrukosti, odnosno Lievoj grupi diskretnog mehaničkog sustava i ambijentalnog fluida. Brzina fluida se dekomponira u vektorsko polje bez vrtložnosti te vektorsko polje bez divergencije korištenjem Helmholtz-Hodge dekompozicije. Značajke vektorskog polja bez vrtložnosti se zatim koriste pri simplektičkoj redukciji multi-fizikalnog sustava za modeliranje dodane inercije krila uronjenog u fluid - važan fenomen za mahokrila insektnog tipa zbog velikih vrijednosti ubrzanja i složene kinematike krila insektnog tipa. Vektorsko polje bez divergencije koristi se za modeliranje viskoznih utjecaja vrtložnim tragom.
- Published
- 2022
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