Orbit-averaged perturbation equations of celestial mechanics with applications to Saturn’s E ring particles

Following Burns 1976, we study the effect of a variety of perturbing forces on a set of orbital elements—semi-major axis a, eccentricity e, inclination i, the longitude of pericenter π, the longitude of the ascending node Ω, and the time of pericenter passage τ. Using elementary dynamics, we can der...

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Main Author: Haanpää, V.-J. (Veli-Jussi)
Format: Others
Language:English
Published: University of Oulu 2018
Subjects:
Online Access:http://urn.fi/URN:NBN:fi:oulu-201812053229
http://nbn-resolving.de/urn:nbn:fi:oulu-201812053229
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spelling ndltd-oulo.fi-oai-oulu.fi-nbnfioulu-2018120532292018-12-06T04:40:09ZOrbit-averaged perturbation equations of celestial mechanics with applications to Saturn’s E ring particlesHaanpää, V.-J. (Veli-Jussi)info:eu-repo/semantics/openAccess© Veli-Jussi Haanpää, 2018PhysicsFollowing Burns 1976, we study the effect of a variety of perturbing forces on a set of orbital elements—semi-major axis a, eccentricity e, inclination i, the longitude of pericenter π, the longitude of the ascending node Ω, and the time of pericenter passage τ. Using elementary dynamics, we can derive the time rates of change of these quantities to produce the perturbation equations of celestial mechanics, which are written in terms of the perturbing forces. If the perturbing forces on a dust particle are small in comparison to a planets gravita- tional attraction, the change in (the first five) orbital elements is slow and on timescales much longer than the dust particle’s orbital period. We can average the effects of perturbations over a single Keplerian orbit (assumed constant). This “orbit-averaging” has both analytical and numerical advantages over non-averaged perturbation equations, which can be seen for example in processing times of computerised orbital models. We can sum the individual perturbation equations of perturbing forces to account for the cumulative effect of all perturbations on an orbital element: 〈dΨ/dt〉_{total} = ∑_{j}〈dΨ/dt〉_{j}, where Ψ is any one of the six osculating orbital elements. These orbit-averaged equations equations are on the order of hundreds of times faster to numerically integrate than the Newtonian equations. To demonstrate the orbit-averaged equations, we can use the orbit-averaged perturbation equations to model paths of dust particles in Saturn’s E Ring. Saturn’s moon Enceladus’ orbit is approximately at the same distance from Saturn as the E Ring, and it has been suggested that the E Ring—made of icy dust—originates from cryovolcanic activity on Enceladus’ south pole. Following Horanyi et al. 1992, we will explore the effects of higher order gravity, radiation pressure, and electromagnetic forces as perturbing forces in the Saturnian system to show the individual effects of perturbing forces on Enceladus-originated ice dust, as well as the cumulative effect of these perturbing forces on orbital equations of the dust.University of Oulu2018-12-05info:eu-repo/semantics/bachelorThesisinfo:eu-repo/semantics/publishedVersionapplication/pdfhttp://urn.fi/URN:NBN:fi:oulu-201812053229urn:nbn:fi:oulu-201812053229eng
collection NDLTD
language English
format Others
sources NDLTD
topic Physics
spellingShingle Physics
Haanpää, V.-J. (Veli-Jussi)
Orbit-averaged perturbation equations of celestial mechanics with applications to Saturn’s E ring particles
description Following Burns 1976, we study the effect of a variety of perturbing forces on a set of orbital elements—semi-major axis a, eccentricity e, inclination i, the longitude of pericenter π, the longitude of the ascending node Ω, and the time of pericenter passage τ. Using elementary dynamics, we can derive the time rates of change of these quantities to produce the perturbation equations of celestial mechanics, which are written in terms of the perturbing forces. If the perturbing forces on a dust particle are small in comparison to a planets gravita- tional attraction, the change in (the first five) orbital elements is slow and on timescales much longer than the dust particle’s orbital period. We can average the effects of perturbations over a single Keplerian orbit (assumed constant). This “orbit-averaging” has both analytical and numerical advantages over non-averaged perturbation equations, which can be seen for example in processing times of computerised orbital models. We can sum the individual perturbation equations of perturbing forces to account for the cumulative effect of all perturbations on an orbital element: 〈dΨ/dt〉_{total} = ∑_{j}〈dΨ/dt〉_{j}, where Ψ is any one of the six osculating orbital elements. These orbit-averaged equations equations are on the order of hundreds of times faster to numerically integrate than the Newtonian equations. To demonstrate the orbit-averaged equations, we can use the orbit-averaged perturbation equations to model paths of dust particles in Saturn’s E Ring. Saturn’s moon Enceladus’ orbit is approximately at the same distance from Saturn as the E Ring, and it has been suggested that the E Ring—made of icy dust—originates from cryovolcanic activity on Enceladus’ south pole. Following Horanyi et al. 1992, we will explore the effects of higher order gravity, radiation pressure, and electromagnetic forces as perturbing forces in the Saturnian system to show the individual effects of perturbing forces on Enceladus-originated ice dust, as well as the cumulative effect of these perturbing forces on orbital equations of the dust.
author Haanpää, V.-J. (Veli-Jussi)
author_facet Haanpää, V.-J. (Veli-Jussi)
author_sort Haanpää, V.-J. (Veli-Jussi)
title Orbit-averaged perturbation equations of celestial mechanics with applications to Saturn’s E ring particles
title_short Orbit-averaged perturbation equations of celestial mechanics with applications to Saturn’s E ring particles
title_full Orbit-averaged perturbation equations of celestial mechanics with applications to Saturn’s E ring particles
title_fullStr Orbit-averaged perturbation equations of celestial mechanics with applications to Saturn’s E ring particles
title_full_unstemmed Orbit-averaged perturbation equations of celestial mechanics with applications to Saturn’s E ring particles
title_sort orbit-averaged perturbation equations of celestial mechanics with applications to saturn’s e ring particles
publisher University of Oulu
publishDate 2018
url http://urn.fi/URN:NBN:fi:oulu-201812053229
http://nbn-resolving.de/urn:nbn:fi:oulu-201812053229
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