Statistical Testing of Dynamical Models Against the Real Kuiper Belt Samantha Lawler, J
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Col-OSSOS: Compositional Homogeneity of Three Kuiper Belt Binaries Michael Marsset, Wesley Fraser, Michele Bannister, Megan Schwamb, Rosemary Pike, Susan Benecchi, J
Col-OSSOS: Compositional Homogeneity of Three Kuiper Belt Binaries Michael Marsset, Wesley Fraser, Michele Bannister, Megan Schwamb, Rosemary Pike, Susan Benecchi, J. Kavelaars, Mike Alexandersen, Ying-Tung Chen, Brett Gladman, et al. To cite this version: Michael Marsset, Wesley Fraser, Michele Bannister, Megan Schwamb, Rosemary Pike, et al.. Col- OSSOS: Compositional Homogeneity of Three Kuiper Belt Binaries. The Planetary Science Journal, IOP Science, 2020, 1 (1), pp.16. 10.3847/PSJ/ab8cc0. hal-02884321 HAL Id: hal-02884321 https://hal.archives-ouvertes.fr/hal-02884321 Submitted on 17 Dec 2020 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. Distributed under a Creative Commons Attribution| 4.0 International License The Planetary Science Journal, 1:16 (9pp), 2020 June https://doi.org/10.3847/PSJ/ab8cc0 © 2020. The Author(s). Published by the American Astronomical Society. Col-OSSOS: Compositional Homogeneity of Three Kuiper Belt Binaries Michaël Marsset1,2 , Wesley C. Fraser2 , Michele T. Bannister3 , Megan E. Schwamb2,4 , Rosemary E Pike5,6 , -
Case File Copy
NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Technical Report 32-7360 Periodic Orbits in fh e Ell@tic Res f~icted Three-Body Problem CASE FILE COPY JET PROPULSION LABORATORY CALIFORNIA INSTITUTE OF TECHNOLOGY PASADENA, CALIFORNIA July 15, 1 969 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION Technical Report 32-1360 Periodic Orbifs in the Elliptic Res tiicted Three-Body Problem R. A. Broucke JET PROPULSION LABORATORY CALIFORNIA INSTITUTE OF TECHNOLOGY PASADENA, CALIFORNIA July 15, 1969 Prepared Under Contract No. NAS 7-100 National Aeronautics and Space Administration Preface The work described in this report was performed by the Mission AnaIysis Division of the Jet Propulsion Laboratory during the period from July 1, 1967 to June 30, 1963. JPL TECHNICAL REPORT 32- 1360 iii Acknowledgment The author wishes to thank several persons with whom he has had constructive conversations concerning the work presented here. In particular, some of the ideas expressed by Dr. A. Deprit of Boeing, Seattle, are at the origin of the work. ilt JPL, special thanks are due to Harry Lass and Carleton Solloway, with whom the problem of the stability of orbits has been discussed in depth. Thanks are also due to Dr. C. Lawson, who has provided the necessary programs for the differential corrections with a least-squares approach, thus avoiding numerical cliKiculties associated with nearly singular matrices; and to Georgia Dvornychenko, who has done much of the programming and computer runs. JPL TECHNICAL REPORT 32-7360 Contents I. Introduction ................ 1 II . Equations of Motion .............. 3 A . The Underlying Two-Body Problem ......... 3 B. Inertial Barycentric Equations of Motion of the Satellite . -
The Onset of Chaos in Permanently Deformed Binaries from Spin–Orbit and Spin–Spin Coupling
The Astrophysical Journal, 913:31 (19pp), 2021 May 20 https://doi.org/10.3847/1538-4357/abf248 © 2021. The American Astronomical Society. All rights reserved. The Onset of Chaos in Permanently Deformed Binaries from Spin–Orbit and Spin–Spin Coupling Darryl Seligman1 and Konstantin Batygin2 1 Dept. of the Geophysical Sciences, University of Chicago, Chicago, IL 60637, USA; [email protected] 2 Division of Geological and Planetary Sciences, Caltech, Pasadena, CA 91125, USA Received 2020 September 16; revised 2021 March 22; accepted 2021 March 24; published 2021 May 21 Abstract Permanently deformed objects in binary systems can experience complex rotation evolution, arising from the extensively studied effect of spin–orbit coupling as well as more nuanced dynamics arising from spin–spin interactions. The ability of an object to sustain an aspheroidal shape largely determines whether or not it will exhibit nontrivial rotational behavior. In this work, we adopt a simplified model of a gravitationally interacting primary and satellite pair, where each body’s quadrupole moment is approximated by two diametrically opposed point masses. After calculating the net gravitational torque on the satellite from the primary, as well as the associated equations of motion, we employ a Hamiltonian formalism that allows for a perturbative treatment of the spin–orbit and retrograde and prograde spin–spin coupling states. By analyzing the resonances individually and collectively, we determine the criteria for resonance overlap and the onset of chaos, as a function of orbital and geometric properties of the binary. We extend the 2D planar geometry to calculate the obliquity evolution. This calculation indicates that satellites in spin–spin resonances undergo precession when inclined out of the plane, but they do not tumble. -
Collision Probabilities in the Edgeworth-Kuiper Belt
Draft version April 30, 2021 Typeset using LATEX default style in AASTeX63 Collision Probabilities in the Edgeworth-Kuiper belt Abedin Y. Abedin,1 JJ Kavelaars,1 Sarah Greenstreet,2, 3 Jean-Marc Petit,4 Brett Gladman,5 Samantha Lawler,6 Michele Bannister,7 Mike Alexandersen,8 Ying-Tung Chen,9 Stephen Gwyn,1 and Kathryn Volk10 1National Research Council of Canada, Herzberg Astronomy and Astrophysics, 5071 West Saanich Road, Victoria, BC V9E 2E7, Canada 2B612 Asteroid Institute, 20 Sunnyside Avenue, Suite 427, Mill Valley, CA 94941, USA 3DIRAC Center, Department of Astronomy, University of Washington, 3910 15th Avenue NE, Seattle, WA 98195, USA 4Institut UTINAM, CNRS-UMR 6213, Universit´eBourgogne Franche Comt´eBP 1615, 25010 Besan¸conCedex, France 5Department of Physics and Astronomy, 6224 Agricultural Road, University of British Columbia, Vancouver, British Columbia, Canada 6Campion College and the Department of Physics, University of Regina, Regina SK, S4S 0A2, Canada 7University of Canterbury, Christchurch, New Zealand 8Minor Planet Center, Smithsonian Astrophysical Observatory, 60 Garden Street, Cambridge, MA 02138, US 9Academia Sinica Institute of Astronomy and Astrophysics, Taiwan 10Lunar and Planetary Laboratory, University of Arizona: Tucson, AZ, USA Submitted to AJ ABSTRACT Here, we present results on the intrinsic collision probabilities, PI , and range of collision speeds, VI , as a function of the heliocentric distance, r, in the trans-Neptunian region. The collision speed is one of the parameters, that serves as a proxy to a collisional outcome e.g., complete disruption and scattering of fragments, or formation of crater, where both processes are directly related to the impact energy. We utilize an improved and de-biased model of the trans-Neptunian object (TNO) region from the \Outer Solar System Origins Survey" (OSSOS). -
In-Orbit Maintenance: the Future of the Satellite Industry
MCTP Title: In-Orbit maintenance: the future of the satellite industry Supervised by: Kevin CARILLO Professor in Information Systems Names of the participants Abhishek KRISHNA Muzikayise Clive SKENJANA Viet Hoang DO Ryota YOSHIDA Qingqing WANG Florent RIZZO Toulouse Business School MCTP project: In-Orbit maintenance: The future of the satellite industry 1 MCTP project: In-Orbit maintenance: The future of the satellite industry Acknowledgement We would like to thank our academic supervisor Kevin Carillo for his continued support throughout the project. We also would like to thank the industry players, who through their busy schedule have managed to grant us an opportunity to hear their views on our topic. Sarah Kartalia for all the provocative MCTP lectures that made us grow during this process. Many thanks to Christophe Benaroya and the AeMBA staff who were readily available for their assistance throughout the process of our project. A special word of thanks also goes to our families for their tremendous support over the past 7 months. 2 MCTP project: In-Orbit maintenance: The future of the satellite industry TEAM 3 MCTP project: In-Orbit maintenance: The future of the satellite industry “It is not the strongest of the species that survive, nor the most intelligent, but the one most responsive to change.” - Charles Darwin 4 MCTP project: In-Orbit maintenance: The future of the satellite industry Contents Acknowledgement ........................................................................................................... 2 I. Executive -
The Planetary Report's New Format Former Administra Tor
A Publicafion 01 THE PLANETA SOCIETY o o o o o • 0-e Board ot Directors CARL SAGAN BRUCE MURRAY FROIVI THE President Vice President EDITOR Director. Laboratory for Planetary Professor of Planetary Studies, Cornell University Science, California Institute of Technology LOUIS FRIEOMAN Executive Director HENRY TANNER California Institute THOMAS O. PAIN E of Technology Welcome to The Planetary Report's New Format Former Administra tor. NASA Chairman, National JOSEPH RYAN Commission on Space O'Meiveny & Myers f you're like me, the fIrst thing you do Members' Dialogue. A few issues ago we Board ot Advisors I after picking up a magazine is to thumb asked you to let our Directors and staff DIANE ACKERMAN JOHN M. LOGSDON through it, look at the pictures and see what know your positions on policy issues that poet and author Director. Space POlicy Institute George Washington University topics are covered. If so, you've probably concern The Planetary Society. Your articu ISAAC ASIMOV author HANS MARK noticed that something has changed in The late and thoughtful responses inspired us to Chancel/or. RICHARD BERENDZEN University of Texas System Planetary Report. With this issue we are in make this dialogue a regular feature, so President, American University JAMES MICHENER stituting a new format designed to make the now each page 3 will be devoted to our JACOUES BLAMONT author Scientific Consultant. Centre magazine easier to read, to further involve members' opinions, with a sidebar featur National dHudes Spafiales, MARVIN MINSKY France Donner Professor of Science, ing material concerning the Society and its Massachusetts Institute our members in The Planetary Society's pri RAY BRADBURY of Technology policies culled from other media sources. -
Enabling Effective Exoplanet / Planetary Collaborative Science a White Paper for the Planetary Science and Astrobiology Decadal Survey 2023-2032
Enabling Effective Exoplanet / Planetary Collaborative Science A White Paper for the Planetary Science and Astrobiology Decadal Survey 2023-2032 Mark S. Marley ([email protected] 650-604-0805 NASA Ames Research Center (ARC), Moffett Field CA, USA) Co-authors: Chester ‘Sonny’ Harman (NASA Ames Research Center); Heidi B. Hammel (AURA) Paul K. Byrne (NCSU); Jonathan Fortney (University of California, Santa Cruz); Alberto Accomazzi (Center for Astrophysics | Harvard & Smithsonian); Sarah E. Moran (JHU Earth & Planetary Sciences); M. J. Way (NASA Goddard Institute for Space Studies); Jessie L. Christiansen (NASA Exoplanet Science Inst./IPAC-Caltech); Noam R. Izenberg (JHU Applied Physics Laboratory); Timothy Holt (Univ. of Southern Queensland); Sanaz Vahidinia (BAERI - NASA Ames Research Center); Erika Kohler (NASA Goddard Space Flight Center); Karalee K. Brugman (Arizona State Univ.) Co-signers: Kathleen Mandt (Johns Hopkins Univ. APL); Victoria Meadows (U. Washington); Sarah Horst (JHU); Edwin Kite (University of Chicago); Dawn Gelino (NASA Exoplanet Science Institute/IPAC-Caltech); Britney Schmidt (Georgia Tech); Niki Parenteau (NASA ARC); Giada Arney (NASA GSFC); Julie Moses (SSI); Michael Line (Ariz. State U.); Kimberly Bott (UCR); Leigh N. Fletcher (U. of Leicester); Sarah Stewart (UC Davis); Tim Lichtenberg (Univ. of Oxford); Giada Arney (NASA GSFC); Channon Visscher (Space Science Institute; Dordt University); David Sing (JHU); Nancy Chanover (NMSU); Abel Méndez (Planetary Hab. Lab., UPR); Ed Rivera-Valentín (LPI); Tiffany Kataria (JPL); Chuanfei Dong (Princeton U.); Ryan MacDonald (Cornell U.); Sang- Heon Dan Shim (Ariz. State U.); Sarah Casewell (University of Leicester); Courtney Dressing (UC Berkeley); Aki Roberge (NASA GSFC); Emily Rickman (Univ. of Geneva); Joshua Lothringer (JHU); Ishan Mishra (Cornell Univ.); Ludmila Carone (Max Planck Inst. -
Data Product Specification for the MISR Cloud Motion Vector Product
JPL D-74995 Earth Observing System Data Product Specification for the MISR Cloud Motion Vector Product -Incorporating the Science Data Processing Interface Control Document Kevin Mueller Jet Propulsion Laboratory September 2, 2014 California Institute of Technology JPL D-74995 Multi -angle Imaging SpectroRadiometer (MISR) Data Product Specification for the MISR Cloud Motion Vector Product -Incorporating the Science Data Processing Interface Control Document APPROVALS: David J. Diner MISR Principal Investigator Earl Hansen MISR Project Manager Approval signatures are on file with the MISR Project. To determine the latest released version of this document, consult the MISR web site (http://misr.jpl.nasa.gov). Jet Propulsion Laboratory September 2, 2014 California Institute of Technology JPL D-74995 Data Product Specification for the MISR Cloud Motion Vector Product Copyright 2014 California Institute of Technology. Government sponsorship acknowledged. The research described in this publication was carried out at the Jet Propulsion Laboratory, California Institute of Technology, under a contract with the National Aeronautics and Space Administration. i JPL D-74995 Data Product Specification for the MISR Cloud Motion Vector Product Document Change Log Revision Date Affected Portions and Description 16 September 2012 All, original release 2 September 2014 The original document described only the Level 3 CMV product. Descriptions of the Level 2 NRT CMV product have been added, including information comparing/contrasting the two product variations. Which Product Versions Does this Document Cover? Product Filename ESDT Version Number Brief Prefix (short names) Description MISR_AM1_CMV MI2CMVPR F01_0001 Level 2 Cloud MI2CMVBR Motion Vectors MI3MCMVN F02_0002 Level 3 Cloud MI3QCMVN Motion Vectors MI3YCMVN ii JPL D-74995 Data Product Specification for the MISR Cloud Motion Vector Product TABLE OF CONTENTS 1 INTRODUCTION ..................................................................................................................................................... -
Arxiv:2001.11605V1 [Astro-Ph.EP] 30 Jan 2020 Formation Process from Systems Other Than Our Own
Draft version February 3, 2020 Typeset using LATEX twocolumn style in AASTeX63 Interstellar comet 2I/Borisov as seen by MUSE: C2, NH2 and red CN detections Michele T. Bannister,1, 2 Cyrielle Opitom,3, 4 Alan Fitzsimmons,1 Youssef Moulane,3, 5, 6 Emmanuel Jehin,5 Darryl Seligman,7 Philippe Rousselot,8 Matthew M. Knight,9, 10 Michael Marsset,11 Megan E. Schwamb,1 Aurelie´ Guilbert-Lepoutre,12 Laurent Jorda,13 Pierre Vernazza,13 and Zouhair Benkhaldoun6 1Astrophysics Research Centre, School of Mathematics and Physics, Queen's University Belfast, Belfast BT7 1NN, United Kingdom 2School of Physical and Chemical Sciences { Te Kura Mat¯u,University of Canterbury, Private Bag 4800, Christchurch 8140, New Zealand 3ESO (European Southern Observatory) - Alonso de Cordova 3107, Vitacura, Santiago Chile 4Institute for Astronomy, University of Edinburgh, Royal Observatory, Edinburgh EH9 3HJ, UK 5STAR Institute, Universit´ede Li`ege,All´eedu 6 aout, 19C, 4000 Li`ege,Belgium 6Oukaimeden Observatory, Cadi Ayyad University, Marrakech, Morocco 7Department of Astronomy, Yale University, 52 Hillhouse Ave., New Haven, CT 06517 8Institut UTINAM UMR 6213, CNRS, Univ. Bourgogne Franche-Comt, OSU THETA, BP 1615, 25010 Besanon Cedex, France 9Department of Physics, United States Naval Academy, 572C Holloway Rd, Annapolis, MD 21402, USA 10University of Maryland, Department of Astronomy, College Park, MD 20742, USA 11Department of Earth, Atmospheric and Planetary Sciences, MIT, 77 Massachusetts Avenue, Cambridge, MA 02139, USA 12Laboratoire de G´eologie de Lyon, LGL-TPE, UMR 5276 CNRS / Universit´ede Lyon / Universit´eClaude Bernard Lyon 1 / ENS Lyon, 69622 Villeurbanne, France 13Aix Marseille Univ, CNRS, LAM, Laboratoire d'Astrophysique de Marseille, Marseille, France (Received 29 Jan 2020; Revised; Accepted) Submitted to ApJ Letters ABSTRACT We report the clear detection of C2 and of abundant NH2 in the first prominently active interstellar comet, 2I/Borisov. -
Statistical Testing of Dynamical Models Against the Real Kuiper Belt
OSSOS: X. How to Use a Survey Simulator: Statistical Testing of Dynamical Models Against the Real Kuiper Belt Lawler, S. M., Kavelaars, J. J., Alexandersen, M., Bannister, M. T., Gladman, B., Petit, J-M., & Shankman, C. (2018). OSSOS: X. How to Use a Survey Simulator: Statistical Testing of Dynamical Models Against the Real Kuiper Belt. Frontiers in Astronomy and Space Sciences, 5, [14]. https://doi.org/10.3389/fspas.2018.00014 Published in: Frontiers in Astronomy and Space Sciences Document Version: Publisher's PDF, also known as Version of record Queen's University Belfast - Research Portal: Link to publication record in Queen's University Belfast Research Portal Publisher rights Copyright 2018 the authors. This is an open access article published under a Creative Commons Attribution License (https://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution and reproduction in any medium, provided the author and source are cited. General rights Copyright for the publications made accessible via the Queen's University Belfast Research Portal is retained by the author(s) and / or other copyright owners and it is a condition of accessing these publications that users recognise and abide by the legal requirements associated with these rights. Take down policy The Research Portal is Queen's institutional repository that provides access to Queen's research output. Every effort has been made to ensure that content in the Research Portal does not infringe any person's rights, or applicable UK laws. If you discover content in the Research Portal that you believe breaches copyright or violates any law, please contact [email protected]. -
Circular Orbit
Circular orbit A circular orbit is the orbit with a fixed distance around the barycenter, that is, in the shape of a circle. Below we consider a circular orbit in astrodynamics or celestial mechanics under standard assumptions. Here the centripetal force is the gravitational force, and the axis mentioned above is the line through the center of the central mass perpendicular to the plane of motion. In this case, not only the distance, but also the speed, angular speed, potential and kinetic energy are constant. There is no periapsis or apoapsis. This orbit has no radial version. A circular orbit is depicted in the top-left Contents quadrant of this diagram, where the Circular acceleration gravitational potential well of the central mass shows potential energy, and the Velocity kinetic energy of the orbital speed is Equation of motion shown in red. The height of the kinetic Angular speed and orbital period energy remains constant throughout the constant speed circular orbit. Energy Delta-v to reach a circular orbit Orbital velocity in general relativity Derivation See also Circular acceleration Transverse acceleration (perpendicular to velocity) causes change in direction. If it is constant in magnitude and changing in direction with the velocity, we get a circular motion. For this centripetal acceleration we have where: is orbital velocity of orbiting body, is radius of the circle is angular speed, measured in radians per unit time. The formula is dimensionless, describing a ratio true for all units of measure applied uniformly across the formula. If the numerical value of is measured in meters per second per second, then the numerical values for will be in meters per second, in meters, and in radians per second. -
Characterising Exoplanets Satellite Arxiv:1310.7800V1 [Astro-Ph.IM] 29 Oct 2013
Master Thesis CHaracterising ExOPlanets Satellite Simulation of Stray Light Contamination on CHEOPS Detector Thibault Kuntzer thibault.kuntzer@epfl.ch Master Thesis Carried out at the University of Bern in the Theoretical Astrophysics and Planetary Science Group Supervised by Advised by Dr. Andrea Fortier Prof. Willy Benz [email protected] [email protected] arXiv:1310.7800v1 [astro-ph.IM] 29 Oct 2013 Followed at EPFL by Prof. Georges Meylan georges.meylan@epfl.ch Spring Semester 2013 Kuntzer, T. Simulation of Stray Light Contamination page | ii Simulation of Stray Light Contamination Kuntzer, T. Abstract he aim of this work is to quantify the amount of Earth stray light that reaches the CHEOPS (CHaracteris- Ting ExOPlanets Satellite) detector. This mission is the first small-class satellite selected by the European Space Agency. It will carry out follow-up measurements on transiting planets. This requires exquisite data that can be acquired only by a space-borne observatory and by well understood and mitigated sources of noise. Earth stray light is one of them which becomes the most prominent noise for faint stars. A software suite was developed to evaluate the contamination by the stray light. As the satellite will be launched in late 2017, the year 2018 is analysed for three different altitudes. Given an visible region at any time, the stray light contamination is simulated at the entrance of the telescope. The amount that reaches the detector is, however, much lower, as it is reduced by the point source transmittance function (PST). It is considered that the exclusion angle subtend by the line of sight to the Sun must be greater than 120°, 35° to the limb of the Earth and 5° away from the limb of the Moon.