Stellar Motion Near the Supermassive Black Hole in the Galactic Center
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Low Thrust Manoeuvres to Perform Large Changes of RAAN Or Inclination in LEO
Facoltà di Ingegneria Corso di Laurea Magistrale in Ingegneria Aerospaziale Master Thesis Low Thrust Manoeuvres To Perform Large Changes of RAAN or Inclination in LEO Academic Tutor: Prof. Lorenzo CASALINO Candidate: Filippo GRISOT July 2018 “It is possible for ordinary people to choose to be extraordinary” E. Musk ii Filippo Grisot – Master Thesis iii Filippo Grisot – Master Thesis Acknowledgments I would like to address my sincere acknowledgments to my professor Lorenzo Casalino, for your huge help in these moths, for your willingness, for your professionalism and for your kindness. It was very stimulating, as well as fun, working with you. I would like to thank all my course-mates, for the time spent together inside and outside the “Poli”, for the help in passing the exams, for the fun and the desperation we shared throughout these years. I would like to especially express my gratitude to Emanuele, Gianluca, Giulia, Lorenzo and Fabio who, more than everyone, had to bear with me. I would like to also thank all my extra-Poli friends, especially Alberto, for your support and the long talks throughout these years, Zach, for being so close although the great distance between us, Bea’s family, for all the Sundays and summers spent together, and my soccer team Belfiga FC, for being the crazy lovable people you are. A huge acknowledgment needs to be address to my family: to my grandfather Luciano, for being a great friend; to my grandmother Bianca, for teaching me what “fighting” means; to my grandparents Beppe and Etta, for protecting me -
Arxiv:2011.13376V1 [Astro-Ph.EP] 26 Nov 2020 Welsh Et Al
On the estimation of circumbinary orbital properties Benjamin C. Bromley Department of Physics & Astronomy, University of Utah, 115 S 1400 E, Rm 201, Salt Lake City, UT 84112 [email protected] Scott J. Kenyon Smithsonian Astrophysical Observatory, 60 Garden St., Cambridge, MA 02138 [email protected] ABSTRACT We describe a fast, approximate method to characterize the orbits of satellites around a central binary in numerical simulations. A goal is to distinguish the free eccentricity | random motion of a satellite relative to a dynamically cool orbit | from oscillatory modes driven by the central binary's time-varying gravitational potential. We assess the performance of the method using the Kepler-16, Kepler-47, and Pluto-Charon systems. We then apply the method to a simulation of orbital damping in a circumbinary environment, resolving relative speeds between small bodies that are slow enough to promote mergers and growth. These results illustrate how dynamical cooling can set the stage for the formation of Tatooine-like planets around stellar binaries and the small moons around the Pluto-Charon binary planet. Subject headings: planets and satellites: formation { planets and satellites: individual: Pluto 1. Introduction Planet formation seems inevitable around nearly all stars. Even the rapidly changing gravitational field around a binary does not prevent planets from settling there (e.g., Armstrong et al. 2014). Recent observations have revealed stable planets around binaries involving main sequence stars (e.g., Kepler-16; Doyle et al. 2011), as well as evolved compact stars (the neutron star-white dwarf binary PSR B1620- 26; Sigurdsson et al. 2003). The Kepler mission (Borucki et al. -
Divinus Lux Observatory Bulletin: Report #28 100 Dave Arnold
Vol. 9 No. 2 April 1, 2013 Journal of Double Star Observations Page Journal of Double Star Observations VOLUME 9 NUMBER 2 April 1, 2013 Inside this issue: Using VizieR/Aladin to Measure Neglected Double Stars 75 Richard Harshaw BN Orionis (TYC 126-0781-1) Duplicity Discovery from an Asteroidal Occultation by (57) Mnemosyne 88 Tony George, Brad Timerson, John Brooks, Steve Conard, Joan Bixby Dunham, David W. Dunham, Robert Jones, Thomas R. Lipka, Wayne Thomas, Wayne H. Warren Jr., Rick Wasson, Jan Wisniewski Study of a New CPM Pair 2Mass 14515781-1619034 96 Israel Tejera Falcón Divinus Lux Observatory Bulletin: Report #28 100 Dave Arnold HJ 4217 - Now a Known Unknown 107 Graeme L. White and Roderick Letchford Double Star Measures Using the Video Drift Method - III 113 Richard L. Nugent, Ernest W. Iverson A New Common Proper Motion Double Star in Corvus 122 Abdul Ahad High Speed Astrometry of STF 2848 With a Luminera Camera and REDUC Software 124 Russell M. Genet TYC 6223-00442-1 Duplicity Discovery from Occultation by (52) Europa 130 Breno Loureiro Giacchini, Brad Timerson, Tony George, Scott Degenhardt, Dave Herald Visual and Photometric Measurements of a Selected Set of Double Stars 135 Nathan Johnson, Jake Shellenberger, Elise Sparks, Douglas Walker A Pixel Correlation Technique for Smaller Telescopes to Measure Doubles 142 E. O. Wiley Double Stars at the IAU GA 2012 153 Brian D. Mason Report on the Maui International Double Star Conference 158 Russell M. Genet International Association of Double Star Observers (IADSO) 170 Vol. 9 No. 2 April 1, 2013 Journal of Double Star Observations Page 75 Using VizieR/Aladin to Measure Neglected Double Stars Richard Harshaw Cave Creek, Arizona [email protected] Abstract: The VizierR service of the Centres de Donnes Astronomiques de Strasbourg (France) offers amateur astronomers a treasure trove of resources, including access to the most current version of the Washington Double Star Catalog (WDS) and links to tens of thousands of digitized sky survey plates via the Aladin Java applet. -
Gravity Recovery by Kinematic State Vector Perturbation from Satellite-To-Satellite Tracking for GRACE-Like Orbits Over Long Arcs
Gravity Recovery by Kinematic State Vector Perturbation from Satellite-to-Satellite Tracking for GRACE-like Orbits over Long Arcs by Nlingilili Habana Report No. 514 Geodetic Science The Ohio State University Columbus, Ohio 43210 January 2020 Gravity Recovery by Kinematic State Vector Perturbation from Satellite-to-Satellite Tracking for GRACE-like Orbits over Long Arcs By Nlingilili Habana Report No. 514 Geodetic Science The Ohio State University Columbus, Ohio 43210 January 2020 Copyright by Nlingilili Habana 2020 Preface This report was prepared for and submitted to the Graduate School of The Ohio State University as a dissertation in partial fulfillment of the requirements for the Degree of Doctor of Philosophy ii Abstract To improve on the understanding of Earth dynamics, a perturbation theory aimed at geopotential recovery, based on purely kinematic state vectors, is implemented. The method was originally proposed in the study by Xu (2008). It is a perturbation method based on Cartesian coordinates that is not subject to singularities that burden most conventional methods of gravity recovery from satellite-to-satellite tracking. The principal focus of the theory is to make the gravity recovery process more efficient, for example, by reducing the number of nuisance parameters associated with arc endpoint conditions in the estimation process. The theory aims to do this by maximizing the benefits of pure kinematic tracking by GNSS over long arcs. However, the practical feasibility of this theory has never been tested numerically. In this study, the formulation of the perturbation theory is first modified to make it numerically practicable. It is then shown, with realistic simulations, that Xu’s original goal of an iterative solution is not achievable under the constraints imposed by numerical integration error. -
Patched Conic Approximation), Ballistic Capture Method [16]
U.P.B. Sci. Bull., Series D, Vol. 81 Iss.1, 2019 ISSN 1454-2358 AUTOMATIC CONTROL OF A SPACECRAFT TRANSFER TRAJECTORY FROM AN EARTH ORBIT TO A MOON ORBIT Florentin-Alin BUŢU1, Romulus LUNGU2 The paper addresses a Spacecraft transfer from an elliptical orbit around the Earth to a circular orbit around the Moon. The geometric parameters of the transfer trajectory are computed, consisting of two orbital arcs, one elliptical and one hyperbolic. Then the state equations are set, describing the dynamics of the three bodies (Spacecraft, Earth and Moon) relative to the Sun. A nonlinear control law (orbit controller) is designed and the parameters of the reference orbit are computed (for each orbital arc);The MATLAB/Simulink model of the automatic control system is designed and with this, by numerical simulation, the transfer path (composed of the two orbit arcs) of the Spacecraft is plotted relative to the Earth and relative to the Moon, the evolution of the Keplerian parameters, the components of the position and velocity vector errors relative to the reference trajectory, as well as the components of the command vector. Keywords: elliptical orbit, nonlinear control, reference orbit. 1. Introduction Considering that the Spacecraft (S) runs an elliptical orbit, with Earth (P) located in one of the ellipse foci, the S transfer over a circular orbit around the Moon (L) is done by traversing a trajectory composed of two orbital arcs, one elliptical and one hyperbolic. From the multitude of papers studied on this topic in order to elaborate the present paper, we mention mainly the following [1] - [15]. -
A Gas Cloud on Its Way Towards the Super-Massive Black Hole in the Galactic Centre
1 A gas cloud on its way towards the super-massive black hole in the Galactic Centre 1 1,2 1 3 4 4,1 5 S.Gillessen , R.Genzel , T.K.Fritz , E.Quataert , C.Alig , A.Burkert , J.Cuadra , F.Eisenhauer1, O.Pfuhl1, K.Dodds-Eden1, C.F.Gammie6 & T.Ott1 1Max-Planck-Institut für extraterrestrische Physik (MPE), Giessenbachstr.1, D-85748 Garching, Germany ( [email protected], [email protected] ) 2Department of Physics, Le Conte Hall, University of California, 94720 Berkeley, USA 3Department of Astronomy, University of California, 94720 Berkeley, USA 4Universitätssternwarte der Ludwig-Maximilians-Universität, Scheinerstr. 1, D-81679 München, Germany 5Departamento de Astronomía y Astrofísica, Pontificia Universidad Católica de Chile, Vicuña Mackenna 4860, 7820436 Macul, Santiago, Chile 6Center for Theoretical Astrophysics, Astronomy and Physics Departments, University of Illinois at Urbana-Champaign, 1002 West Green St., Urbana, IL 61801, USA Measurements of stellar orbits1-3 provide compelling evidence4,5 that the compact radio source Sagittarius A* at the Galactic Centre is a black hole four million times the mass of the Sun. With the exception of modest X-ray and infrared flares6,7, Sgr A* is surprisingly faint, suggesting that the accretion rate and radiation efficiency near the event horizon are currently very low3,8. Here we report the presence of a dense gas cloud approximately three times the mass of Earth that is falling into the accretion zone of Sgr A*. Our observations tightly constrain the cloud’s orbit to be highly eccentric, with an innermost radius of approach of only ~3,100 times the event horizon that will be reached in 2013. -
Terrestrial Planets in High-Mass Disks Without Gas Giants
A&A 557, A42 (2013) Astronomy DOI: 10.1051/0004-6361/201321304 & c ESO 2013 Astrophysics Terrestrial planets in high-mass disks without gas giants G. C. de Elía, O. M. Guilera, and A. Brunini Facultad de Ciencias Astronómicas y Geofísicas, Universidad Nacional de La Plata and Instituto de Astrofísica de La Plata, CCT La Plata-CONICET-UNLP, Paseo del Bosque S/N, 1900 La Plata, Argentina e-mail: [email protected] Received 15 February 2013 / Accepted 24 May 2013 ABSTRACT Context. Observational and theoretical studies suggest that planetary systems consisting only of rocky planets are probably the most common in the Universe. Aims. We study the potential habitability of planets formed in high-mass disks without gas giants around solar-type stars. These systems are interesting because they are likely to harbor super-Earths or Neptune-mass planets on wide orbits, which one should be able to detect with the microlensing technique. Methods. First, a semi-analytical model was used to define the mass of the protoplanetary disks that produce Earth-like planets, super- Earths, or mini-Neptunes, but not gas giants. Using mean values for the parameters that describe a disk and its evolution, we infer that disks with masses lower than 0.15 M are unable to form gas giants. Then, that semi-analytical model was used to describe the evolution of embryos and planetesimals during the gaseous phase for a given disk. Thus, initial conditions were obtained to perform N-body simulations of planetary accretion. We studied disks of 0.1, 0.125, and 0.15 M. -
Mètodes De Detecció I Anàlisi D'exoplanetes
MÈTODES DE DETECCIÓ I ANÀLISI D’EXOPLANETES Rubén Soussé Villa 2n de Batxillerat Tutora: Dolors Romero IES XXV Olimpíada 13/1/2011 Mètodes de detecció i anàlisi d’exoplanetes . Índex - Introducció ............................................................................................. 5 [ Marc Teòric ] 1. L’Univers ............................................................................................... 6 1.1 Les estrelles .................................................................................. 6 1.1.1 Vida de les estrelles .............................................................. 7 1.1.2 Classes espectrals .................................................................9 1.1.3 Magnitud ........................................................................... 9 1.2 Sistemes planetaris: El Sistema Solar .............................................. 10 1.2.1 Formació ......................................................................... 11 1.2.2 Planetes .......................................................................... 13 2. Planetes extrasolars ............................................................................ 19 2.1 Denominació .............................................................................. 19 2.2 Història dels exoplanetes .............................................................. 20 2.3 Mètodes per detectar-los i saber-ne les característiques ..................... 26 2.3.1 Oscil·lació Doppler ........................................................... 27 2.3.2 Trànsits -
En Interaktiv Visualisering Av Data Och Upptäcktsmetoder Karin Reidarman
LIU-ITN-TEK-A-018/045--SE Exoplaneter: En Interaktiv Visualisering av Data och Upptäcktsmetoder Karin Reidarman 2018-11-30 Department of Science and Technology Institutionen för teknik och naturvetenskap Linköping University Linköpings universitet nedewS ,gnipökrroN 47 106-ES 47 ,gnipökrroN nedewS 106 47 gnipökrroN LIU-ITN-TEK-A-018/045--SE Exoplaneter: En Interaktiv Visualisering av Data och Upptäcktsmetoder Examensarbete utfört i Medieteknik vid Tekniska högskolan vid Linköpings universitet Karin Reidarman Handledare Emil Axelsson Examinator Anders Ynnerman Norrköping 2018-11-30 Upphovsrätt Detta dokument hålls tillgängligt på Internet – eller dess framtida ersättare – under en längre tid från publiceringsdatum under förutsättning att inga extra- ordinära omständigheter uppstår. Tillgång till dokumentet innebär tillstånd för var och en att läsa, ladda ner, skriva ut enstaka kopior för enskilt bruk och att använda det oförändrat för ickekommersiell forskning och för undervisning. Överföring av upphovsrätten vid en senare tidpunkt kan inte upphäva detta tillstånd. All annan användning av dokumentet kräver upphovsmannens medgivande. För att garantera äktheten, säkerheten och tillgängligheten finns det lösningar av teknisk och administrativ art. Upphovsmannens ideella rätt innefattar rätt att bli nämnd som upphovsman i den omfattning som god sed kräver vid användning av dokumentet på ovan beskrivna sätt samt skydd mot att dokumentet ändras eller presenteras i sådan form eller i sådant sammanhang som är kränkande för upphovsmannens litterära eller konstnärliga anseende eller egenart. För ytterligare information om Linköping University Electronic Press se förlagets hemsida http://www.ep.liu.se/ Copyright The publishers will keep this document online on the Internet - or its possible replacement - for a considerable time from the date of publication barring exceptional circumstances. -
Spacecraft Conjunction Assessment and Collision Avoidance Best Practices Handbook
National Aeronautics and Space Administration National Aeronautics and Space Administration NASA Spacecraft Conjunction Assessment and Collision Avoidance Best Practices Handbook December 2020 NASA/SP-20205011318 The cover photo is an image from the Hubble Space Telescope showing galaxies NGC 4038 and NGC 4039, also known as the Antennae Galaxies, locked in a deadly embrace. Once normal spiral galaxies, the pair have spent the past few hundred million years sparring with one another. Image can be found at: https://images.nasa.gov/details-GSFC_20171208_Archive_e001327 ii NASA Spacecraft Conjunction Assessment and Collision Avoidance Best Practices Handbook DOCUMENT HISTORY LOG Status Document Effective Description (Baseline/Revision/ Version Date Canceled) Baseline V0 iii NASA Spacecraft Conjunction Assessment and Collision Avoidance Best Practices Handbook THIS PAGE INTENTIONALLY LEFT BLANK iv NASA Spacecraft Conjunction Assessment and Collision Avoidance Best Practices Handbook Table of Contents Preface ................................................................................................................ 1 1. Introduction ................................................................................................... 3 2. Roles and Responsibilities ............................................................................ 5 3. History ........................................................................................................... 7 USSPACECOM CA Process ............................................................. -
Modelling a Group-Scale Lens at Z ∼ 0.6 ∗
UNIVERSIDADE FEDERAL DO RIO GRANDE DO SUL PROGRAMA DE POS-GRADUAC¸´ AO~ EM F´ISICA INSTITUTO DE F´ISICA Modelling a group-scale lens at z ∼ 0:6 ∗ M^onicaTergolina Disserta¸c~ao realizada sob orienta¸c~ao da Professora Dra. Cristina Furlanetto e da Professora Dra. Marina Trevisan e apre- sentada ao Instituto de F´ısicada UFRGS em preenchimento parcial dos requisitos para a obten¸c~aodo t´ıtulo de Mestre em F´ısica. Porto Alegre, Mar¸code 2020. ∗Trabalho financiado pela Coordena¸c~aode Aperfei¸coamento de Pessoal de N´ıvel Superior (CAPES). Para meus amados pais, av´o e irm~a,essenciais na minha vida. Agradecimentos Primeiramente, gostaria de agradecer a minha m~aee meu pai, Fl´aviae Claudio, por sempre me incentivarem a ir atr´asdos meus sonhos e por terem me proporcionado a oportunidade de estudar na UFRGS. Sou muito grata por todo apoio e amor incondicional que recebi de voc^es,da minha irm~aMaria Alice e a minha av´oZilah. Agrade¸coao meu amor Henrique, por todo amor, paci^encia,compreens~ao,carinho e cuidado. Tua companhia foi essencial para que eu finalizasse esse trabalho. Queria agradecer aos meus cachorros, Mocki, Bacon, Costelinha e Minnie pelo amor e pelo constante suporte emocional. Voc^esforam fudamentais para manter minha sanidade mental nesse per´ıodo. Sou muito grata `aminha orientadora Profa. Dra. Cristina Furlanetto e `aminha co- orientadora Prof. Dra. Marina Trevisan. Obrigada pela confian¸cadepositada em mim, pelos ensinamentos, conselhos, risadas e por me ajudarem a n~aoentrar em desespero na reta final, voc^esforam incans´aveis. -
The Extreme Luminosity States of Sagittarius A*
A&A 512, A2 (2010) Astronomy DOI: 10.1051/0004-6361/200913186 & c ESO 2010 Astrophysics The extreme luminosity states of Sagittarius A* N. Sabha1, G. Witzel1,A.Eckart1,2, R. M. Buchholz1,M.Bremer1, R. Gießübel2,1, M. García-Marín1, D. Kunneriath1,2,K.Muzic1, R. Schödel3, C. Straubmeier1, M. Zamaninasab2,1, and A. Zernickel1 1 I.Physikalisches Institut, Universität zu Köln, Zülpicher Str. 77, 50937 Köln, Germany e-mail: [sabha;witzel;eckart]@ph1.uni-koeln.de 2 Max-Planck-Institut für Radioastronomie, Auf dem Hügel 69, 53121 Bonn, Germany 3 Instituto de Astrofísica de Andalucía (CSIC), Camino Bajo de Huétor 50, 18008 Granada, Spain e-mail: [email protected] Received 26 August 2009 / Accepted 22 December 2009 ABSTRACT We discuss mm-wavelength radio, 2.2–11.8 μm NIR and 2–10 keV X-ray light curves of the super massive black hole (SMBH) coun- terpart of Sagittarius A* (SgrA*) near its lowest and highest observed luminosity states. We investigate the structure and brightness of the central S-star cluster harboring the SMBH to obtain reliable flux density estimates of SgrA* during its low luminosity phases. We then discuss the physical processes responsible for the brightest flare as well as the faintest flare or quiescent emission in the NIR and X-ray domain. To investigate the low state of SgrA* we use three independent methods to remove or strongly suppress the flux density contributions of stars in the central 2 diameter region around SgrA*. The three methods are: a) low-pass filtering the image; b) iterative identification and removal of individual stars; c) automatic point spread function (PSF) subtraction.