Tilting Saturn II. Numerical Model
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
6 Orbit Relative to the Sun. Crossing Times
6 Orbit Relative to the Sun. Crossing Times We begin by studying the position of the orbit and ground track of an arbi- trary satellite relative to the direction of the Sun. We then turn more specif- ically to Sun-synchronous satellites for which this relative position provides the very definition of their orbit. 6.1 Cycle with Respect to the Sun 6.1.1 Crossing Time At a given time, it is useful to know the local time on the ground track, i.e., the LMT, deduced in a straightforward manner from the UT once the longitude of the place is given, using (4.49). The local mean time (LMT) on the ground track at this given time is called the crossing time or local crossing time. To obtain the local apparent time (LAT), one must know the day of the year to specify the equation of time ET. In all matters involving the position of the Sun (elevation and azimuth) relative to a local frame, this is the time that should be used. The ground track of the satellite can be represented by giving the crossing time. We have chosen to represent the LMT using colour on Colour Plates IIb, IIIb and VII to XI. For Sun-synchronous satellites such as MetOp-1, it is clear that the cross- ing time (in the ascending or descending direction) depends only on the latitude. At a given place (except near the poles), one crossing occurs during the day, the other at night. For the HEO of the Ellipso Borealis satellite, the stability of the crossing time also shows up clearly. -
Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur
Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur To cite this version: Alex Soumbatov-Gur. Phobos, Deimos: Formation and Evolution. [Research Report] Karpov institute of physical chemistry. 2019. hal-02147461 HAL Id: hal-02147461 https://hal.archives-ouvertes.fr/hal-02147461 Submitted on 4 Jun 2019 HAL is a multi-disciplinary open access L’archive ouverte pluridisciplinaire HAL, est archive for the deposit and dissemination of sci- destinée au dépôt et à la diffusion de documents entific research documents, whether they are pub- scientifiques de niveau recherche, publiés ou non, lished or not. The documents may come from émanant des établissements d’enseignement et de teaching and research institutions in France or recherche français ou étrangers, des laboratoires abroad, or from public or private research centers. publics ou privés. Phobos, Deimos: Formation and Evolution Alex Soumbatov-Gur The moons are confirmed to be ejected parts of Mars’ crust. After explosive throwing out as cone-like rocks they plastically evolved with density decays and materials transformations. Their expansion evolutions were accompanied by global ruptures and small scale rock ejections with concurrent crater formations. The scenario reconciles orbital and physical parameters of the moons. It coherently explains dozens of their properties including spectra, appearances, size differences, crater locations, fracture symmetries, orbits, evolution trends, geologic activity, Phobos’ grooves, mechanism of their origin, etc. The ejective approach is also discussed in the context of observational data on near-Earth asteroids, main belt asteroids Steins, Vesta, and Mars. The approach incorporates known fission mechanism of formation of miniature asteroids, logically accounts for its outliers, and naturally explains formations of small celestial bodies of various sizes. -
Calibration of the Angular Momenta of the Minor Planets in the Solar System Jian Li1, Zhihong Jeff Xia2, Liyong Zhou1
Astronomy & Astrophysics manuscript no. arXiv c ESO 2019 September 26, 2019 Calibration of the angular momenta of the minor planets in the solar system Jian Li1, Zhihong Jeff Xia2, Liyong Zhou1 1School of Astronomy and Space Science & Key Laboratory of Modern Astronomy and Astrophysics in Ministry of Education, Nanjing University, 163 Xianlin Road, Nanjing 210023, PR China e-mail: [email protected] 2Department of Mathematics, Northwestern University, 2033 Sheridan Road, Evanston, IL 60208, USA e-mail: [email protected] September 26, 2019 ABSTRACT Aims. We aim to determine the relative angle between the total angular momentum of the minor planets and that of the Sun-planets system, and to improve the orientation of the invariable plane of the solar system. Methods. By utilizing physical parameters available in public domain archives, we assigned reasonable masses to 718041 minor plan- ets throughout the solar system, including near-Earth objects, main belt asteroids, Jupiter trojans, trans-Neptunian objects, scattered- disk objects, and centaurs. Then we combined the orbital data to calibrate the angular momenta of these small bodies, and evaluated the specific contribution of the massive dwarf planets. The effects of uncertainties on the mass determination and the observational incompleteness were also estimated. Results. We determine the total angular momentum of the known minor planets to be 1:7817 × 1046 g · cm2 · s−1. The relative angle α between this vector and the total angular momentum of the Sun-planets system is calculated to be about 14:74◦. By excluding the dwarf planets Eris, Pluto, and Haumea, which have peculiar angular momentum directions, the angle α drops sharply to 1:76◦; a similar result applies to each individual minor planet group (e.g., trans-Neptunian objects). -
Some Special Types of Orbits Around Jupiter
aerospace Article Some Special Types of Orbits around Jupiter Yongjie Liu 1, Yu Jiang 1,*, Hengnian Li 1,2,* and Hui Zhang 1 1 State Key Laboratory of Astronautic Dynamics, Xi’an Satellite Control Center, Xi’an 710043, China; [email protected] (Y.L.); [email protected] (H.Z.) 2 School of Electronic and Information Engineering, Xi’an Jiaotong University, Xi’an 710049, China * Correspondence: [email protected] (Y.J.); [email protected] (H.L.) Abstract: This paper intends to show some special types of orbits around Jupiter based on the mean element theory, including stationary orbits, sun-synchronous orbits, orbits at the critical inclination, and repeating ground track orbits. A gravity model concerning only the perturbations of J2 and J4 terms is used here. Compared with special orbits around the Earth, the orbit dynamics differ greatly: (1) There do not exist longitude drifts on stationary orbits due to non-spherical gravity since only J2 and J4 terms are taken into account in the gravity model. All points on stationary orbits are degenerate equilibrium points. Moreover, the satellite will oscillate in the radial and North-South directions after a sufficiently small perturbation of stationary orbits. (2) The inclinations of sun-synchronous orbits are always bigger than 90 degrees, but smaller than those for satellites around the Earth. (3) The critical inclinations are no-longer independent of the semi-major axis and eccentricity of the orbits. The results show that if the eccentricity is small, the critical inclinations will decrease as the altitudes of orbits increase; if the eccentricity is larger, the critical inclinations will increase as the altitudes of orbits increase. -
Orbital Dynamics and Numerical N-Body Simulations of Extrasolar Moons and Giant Planets
ORBITAL DYNAMICS AND NUMERICAL N-BODY SIMULATIONS OF EXTRASOLAR MOONS AND GIANT PLANETS. A Dissertation Presented to the Faculty of the Graduate School of Cornell University in Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy by Yu-Cian Hong August 2019 c 2019 Yu-Cian Hong ALL RIGHTS RESERVED ORBITAL DYNAMICS AND NUMERICAL N-BODY SIMULATIONS OF EXTRASOLAR MOONS AND GIANT PLANETS. Yu-Cian Hong, Ph.D. Cornell University 2019 This thesis work focuses on computational orbital dynamics of exomoons and exoplanets. Exomoons are highly sought-after astrobiological targets. Two can- didates have been discovered to-date (Bennett et al., 2014, Teachey & Kipping, 2018). We developed the first N-body integrator that can handle exomoon orbits in close planet-planet interactions, for the following three projects. (1) Instability of moons around non-oblate planets associated with slowed nodal precession and resonances with stars.This work reversed the commonsensical notion that spinning giant planets should be oblate. Moons around spherical planets were destabilized by 3:2 and 1:1 resonance overlap or the chaotic zone around 1:1 resonance between the orbital precession of the moons and the star. Normally, the torque from planet oblateness keeps the orbit of close-in moons precess fast ( period ∼ 7 yr for Io). Without planet oblateness, Io?s precession period is much longer (∼ 104 yr), which allowed resonance with the star, thus the in- stability. Therefore, realistic treatment of planet oblateness is critical in moon dynamics. (2) Orbital stability of moons in planet-planet scattering. Planet- planet scattering is the best model to date for explaining the eccentricity distri- bution of exoplanets. -
Tilting Ice Giants with a Spin–Orbit Resonance
The Astrophysical Journal, 888:60 (12pp), 2020 January 10 https://doi.org/10.3847/1538-4357/ab5d35 © 2020. The American Astronomical Society. All rights reserved. Tilting Ice Giants with a Spin–Orbit Resonance Zeeve Rogoszinski and Douglas P. Hamilton Astronomy Department, University of Maryland, College Park, MD 20742, USA; [email protected], [email protected] Received 2019 August 28; revised 2019 November 20; accepted 2019 November 26; published 2020 January 8 Abstract Giant collisions can account for Uranus’s and Neptune’s large obliquities, yet generating two planets with widely different tilts and strikingly similar spin rates is a low-probability event. Trapping into a secular spin–orbit resonance, a coupling between spin and orbit precession frequencies, is a promising alternative, as it can tilt the planet without altering its spin period. We show with numerical integrations that if Uranus harbored a massive circumplanetary disk at least three times the mass of its satellite system while it was accreting its gaseous atmosphere, then its spin precession rate would increase enough to resonate with its own orbit, potentially driving the planet’s obliquity to 70°.Wefind that the presence of a massive disk moves the Laplace radius significantly outward from its classical value, resulting in more of the disk contributing to the planet’s pole precession. Although we can generate tilts greater than 70°only rarely and cannot drive tilts beyond 90°, a subsequent collision with an object about 0.5 M⊕ could tilt Uranus from 70°to 98°. Minimizing the masses and number of giant impactors from two or more to just one increases the likelihood of producing Uranus’s spin states by about an order of magnitude. -
Long Term Behavior of a Hypothetical Planet in a Highly Eccentric Orbit
Long term behavior of a hypothetical planet in a highly eccentric orbit R. Nufer,∗ W. Baltensperger,† W. Woelfli‡ March 29, 2018 Abstract crossed this cloud, molecules activating a Green- house effect were produced in the upper atmosphere For a hypothetical planet on a highly eccentric or- in an amount sufficient to transiently enhance the bit, we have calculated the osculating orbital pa- mean surface temperature on Earth. Very close rameters and its closest approaches to Earth and flyby events even resulted in earthquakes and vol- Moon over a period of 750 kyr. The approaches canic activities. In extreme cases, a rotation of the which are close enough to influence the climate of entire Earth relative to its rotation axis occured in the Earth form a pattern comparable to that of the response to the transient strong gravitational inter- past climatic changes, as recorded in deep sea sedi- action. These polar shifts took place with a fre- ments and polar ice cores. quency of about one in one million years on the average. The first of them was responsible for the major drop in mean temperature, whereas the last 1 Motivation one terminated Earth’s Pleistocene Ice Age 11.5 kyr ago. At present, planet Z does not exist any more. The information on Earth’s past climate obtained The high eccentricity of Z’s orbit corresponds to from deep sea sediments and polar ice cores indi- a small orbital angular momentum. This could be cates that the global temperature oscillated with a transferred to one of the inner planets during a close small amplitude around a constant mean value for encounter, so that Z plunged into the sun. -
Simulation of Attitude and Orbital Disturbances Acting on ASPECT Satellite in the Vicinity of the Binary Asteroid Didymos
Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos Erick Flores García Space Engineering, masters level (120 credits) 2017 Luleå University of Technology Department of Computer Science, Electrical and Space Engineering Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos Erick Flores Garcia School of Electrical Engineering Thesis submitted for examination for the degree of Master of Science in Technology. Espoo December 6, 2016 Thesis supervisors: Prof. Jaan Praks Dr. Leonard Felicetti Aalto University Luleå University of Technology School of Electrical Engineering Thesis advisors: M.Sc. Tuomas Tikka M.Sc. Nemanja Jovanović aalto university abstract of the school of electrical engineering master’s thesis Author: Erick Flores Garcia Title: Simulation of attitude and orbital disturbances acting on ASPECT satellite in the vicinity of the binary asteroid Didymos Date: December 6, 2016 Language: English Number of pages: 9+84 Department of Radio Science and Engineering Professorship: Automation Technology Supervisor: Prof. Jaan Praks Advisors: M.Sc. Tuomas Tikka, M.Sc. Nemanja JovanoviÊ Asteroid missions are gaining interest from the scientific community and many new missions are planned. The Didymos binary asteroid is a Near-Earth Object and the target of the Asteroid Impact and Deflection Assessment (AIDA). This joint mission, developed by NASA and ESA, brings the possibility to build one of the first CubeSats for deep space missions: the ASPECT satellite. Navigation systems of a deep space satellite differ greatly from the common planetary missions. Orbital environment close to an asteroid requires a case-by-case analysis. -
Orbital Resonances in the Inner Neptunian System I. the 2:1 Proteus–Larissa Mean-Motion Resonance Ke Zhang ∗, Douglas P
Icarus 188 (2007) 386–399 www.elsevier.com/locate/icarus Orbital resonances in the inner neptunian system I. The 2:1 Proteus–Larissa mean-motion resonance Ke Zhang ∗, Douglas P. Hamilton Department of Astronomy, University of Maryland, College Park, MD 20742, USA Received 1 June 2006; revised 22 November 2006 Available online 20 December 2006 Abstract We investigate the orbital resonant history of Proteus and Larissa, the two largest inner neptunian satellites discovered by Voyager 2.Due to tidal migration, these two satellites probably passed through their 2:1 mean-motion resonance a few hundred million years ago. We explore this resonance passage as a method to excite orbital eccentricities and inclinations, and find interesting constraints on the satellites’ mean density 3 3 (0.05 g/cm < ρ¯ 1.5g/cm ) and their tidal dissipation parameters (Qs > 10). Through numerical study of this mean-motion resonance passage, we identify a new type of three-body resonance between the satellite pair and Triton. These new resonances occur near the traditional two-body resonances between the small satellites and, surprisingly, are much stronger than their two-body counterparts due to Triton’s large mass and orbital inclination. We determine the relevant resonant arguments and derive a mathematical framework for analyzing resonances in this special system. © 2007 Elsevier Inc. All rights reserved. Keywords: Resonances, orbital; Neptune, satellites; Triton; Satellites, dynamics 1. Introduction Most of the debris was probably swept up by Triton (Cuk´ and Gladman, 2005), while some material close to Neptune sur- Prior to the Voyager 2 encounter, large icy Triton and dis- vived to form a new generation of satellites with an accretion tant irregular Nereid were Neptune’s only known satellites. -
Exploring the Orbital Evolution of Planetary Systems
Exploring the orbital evolution of planetary systems Tabar´e Gallardo∗ Instituto de F´ısica, Facultad de Ciencias, Udelar. (Dated: January 22, 2017) The aim of this paper is to encourage the use of orbital integrators in the classroom to discover and understand the long term dynamical evolution of systems of orbiting bodies. We show how to perform numerical simulations and how to handle the output data in order to reveal the dynamical mechanisms that dominate the evolution of arbitrary planetary systems in timescales of millions of years using a simple but efficient numerical integrator. Trough some examples we reveal the fundamental properties of the planetary systems: the time evolution of the orbital elements, the free and forced modes that drive the oscillations in eccentricity and inclination, the fundamental frequencies of the system, the role of the angular momenta, the invariable plane, orbital resonances and the Kozai-Lidov mechanism. To be published in European Journal of Physics. 2 I. INTRODUCTION With few exceptions astronomers cannot make experiments, they are limited to observe the universe. The laboratory for the astronomer usually takes the form of computer simulations. This is the most important instrument for the study of the dynamical behavior of gravitationally interacting bodies. A planetary system, for example, evolves mostly due to gravitation acting over very long timescales generating what is called a secular evolution. This secular evolution can be deduced analytically by means of the theory of perturbations, but can also be explored in the classroom by means of precise numerical integrators. Some facilities exist to visualize and experiment with the gravitational interactions between massive bodies1–3. -
Forced Obliquities and Moments of Inertia of Ceres and Vesta ⇑ B.G
Icarus 213 (2011) 496–509 Contents lists available at ScienceDirect Icarus journal homepage: www.elsevier.com/locate/icarus Forced obliquities and moments of inertia of Ceres and Vesta ⇑ B.G. Bills a, , F. Nimmo b a Jet Propulsion Laboratory, Pasadena, CA 91109, USA b Department of Earth and Planetary Sciences, University of California Santa Cruz, Santa Cruz, CA 95064, USA article info abstract Article history: We examine models of secular variations in the orbit and spin poles of Ceres and Vesta, the two most Received 22 July 2009 massive bodies in the main asteroid belt. If the spin poles are fully damped, then the current values of Revised 30 August 2010 obliquity, or angular separation between spin and orbit poles, are diagnostic of the moments of inertia Accepted 1 September 2010 and thus indicative of the extent of differentiation of these bodies. Using existing shape models and Available online 21 September 2010 assuming uniform density, the present obliquity values are predicted to be 12.31° for Ceres and 15.66° for Vesta. Part of this difference is related to differing orbital inclinations; a more centrally condensed Keywords: internal structure would yield more rapid spin pole precession, and larger obliquity. Time scales for tidal Asteroids, Dynamics damping are expected to be rather long. However, at least for Vesta, current estimates of the spin pole Asteroid Ceres Asteroid Vesta location are consistent with its obliquity being fully damped. When the degree two gravity coefficients Rotational dynamics and spin pole orientations are determined by the Dawn spacecraft, it will allow accurate determination of the moments of inertia of these bodies, assuming the obliquities are damped. -
Astro 250: Solutions to Problem Set 5 by Eugene Chiang
Astro 250: Solutions to Problem Set 5 by Eugene Chiang Problem 1. Precessing Planes and the Invariable Plane Consider a star of mass mc orbited by two planets on nearly circular orbits. The mass and semi-major axis of the inner planet are m1 and a1, respectively, and those of the outer planet, m2 = (1/2) × m1 and a2 = 4 × a1. The mutual inclination between the two orbits is i 1. This problem explores the inclination and nodal behavior of the two planets. a) What is the inclination of each planet with respect to the invariable plane of the system? The invariable plane is perpendicular to the total (vector) angular momentum of all planetary orbits. Neglect the contribution of orbital eccentricity to the angular momentum. Call these inclinations i1 and i2. The masses and semi-major axes of the two planets are so chosen as to make the arithmetic easy;√ the norm of each planet’s angular momentum is the same as the other, |~l1| = |~l2| = m1 Gmca1. Orient the x-y axes in the invariable plane so that the y-axis lies along the line of intersection between the two orbit planes (the nodal line). Then in the x-z plane, the total angular momentum vector lies along the z-axis, while ~l1 lies (say) in quadrant II and makes an angle with respect to the z-axis of i1 > 0, while l~2 lies in quadrant I and makes an angle with respect to the z-axis of i2 > 0. Remember that the mutual inclination i = i1 + i2.