Astrocladistics of the Jovian Trojan Swarms
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Occultation Newsletter Volume 8, Number 4
Volume 12, Number 1 January 2005 $5.00 North Am./$6.25 Other International Occultation Timing Association, Inc. (IOTA) In this Issue Article Page The Largest Members Of Our Solar System – 2005 . 4 Resources Page What to Send to Whom . 3 Membership and Subscription Information . 3 IOTA Publications. 3 The Offices and Officers of IOTA . .11 IOTA European Section (IOTA/ES) . .11 IOTA on the World Wide Web. Back Cover ON THE COVER: Steve Preston posted a prediction for the occultation of a 10.8-magnitude star in Orion, about 3° from Betelgeuse, by the asteroid (238) Hypatia, which had an expected diameter of 148 km. The predicted path passed over the San Francisco Bay area, and that turned out to be quite accurate, with only a small shift towards the north, enough to leave Richard Nolthenius, observing visually from the coast northwest of Santa Cruz, to have a miss. But farther north, three other observers video recorded the occultation from their homes, and they were fortuitously located to define three well- spaced chords across the asteroid to accurately measure its shape and location relative to the star, as shown in the figure. The dashed lines show the axes of the fitted ellipse, produced by Dave Herald’s WinOccult program. This demonstrates the good results that can be obtained by a few dedicated observers with a relatively faint star; a bright star and/or many observers are not always necessary to obtain solid useful observations. – David Dunham Publication Date for this issue: July 2005 Please note: The date shown on the cover is for subscription purposes only and does not reflect the actual publication date. -
On the Accuracy of Restricted Three-Body Models for the Trojan Motion
DISCRETE AND CONTINUOUS Website: http://AIMsciences.org DYNAMICAL SYSTEMS Volume 11, Number 4, December 2004 pp. 843{854 ON THE ACCURACY OF RESTRICTED THREE-BODY MODELS FOR THE TROJAN MOTION Frederic Gabern1, Angel` Jorba1 and Philippe Robutel2 Departament de Matem`aticaAplicada i An`alisi Universitat de Barcelona Gran Via 585, 08007 Barcelona, Spain1 Astronomie et Syst`emesDynamiques IMCCE-Observatoire de Paris 77 Av. Denfert-Rochereau, 75014 Paris, France2 Abstract. In this note we compare the frequencies of the motion of the Trojan asteroids in the Restricted Three-Body Problem (RTBP), the Elliptic Restricted Three-Body Problem (ERTBP) and the Outer Solar System (OSS) model. The RTBP and ERTBP are well-known academic models for the motion of these asteroids, and the OSS is the standard model used for realistic simulations. Our results are based on a systematic frequency analysis of the motion of these asteroids. The main conclusion is that both the RTBP and ERTBP are not very accurate models for the long-term dynamics, although the level of accuracy strongly depends on the selected asteroid. 1. Introduction. The Restricted Three-Body Problem models the motion of a particle under the gravitational attraction of two point masses following a (Keple- rian) solution of the two-body problem (a general reference is [17]). The goal of this note is to discuss the degree of accuracy of such a model to study the real motion of an asteroid moving near the Lagrangian points of the Sun-Jupiter system. To this end, we have considered two restricted three-body problems, namely: i) the Circular RTBP, in which Sun and Jupiter describe a circular orbit around their centre of mass, and ii) the Elliptic RTBP, in which Sun and Jupiter move on an elliptic orbit. -
Comparison of the Physical Properties of the L4 and L5 Trojan Asteroids from ATLAS Data
Draft version January 13, 2021 Typeset using LATEX default style in AASTeX62 Comparison of the physical properties of the L4 and L5 Trojan asteroids from ATLAS data A. McNeill,1 N. Erasmus,2 D.E. Trilling,1, 2 J.P. Emery,1 J. L. Tonry,3 L. Denneau,3 H. Flewelling,3 A. Heinze,3 B. Stalder,4 and H.J. Weiland3 1Department of Astronomy and Planetary Science, Northern Arizona University, Flagstaff, AZ 86011, USA 2South African Astronomical Observatory, Cape Town, 7925, South Africa. 3Institute for Astronomy, University of Hawaii, Honolulu, HI 9682, USA. 4Vera C. Rubin Observatory Project Office, 950 N. Cherry Ave, Tucson, AZ, USA ABSTRACT Jupiter has nearly 8000 known co-orbital asteroids orbiting in the L4 and L5 Lagrange points called Jupiter Trojan asteroids. Aside from the greater number density of the L4 cloud the two clouds are in many ways considered to be identical. Using sparse photometric data taken by the Asteroid Terrestrial-impact Last Alert System (ATLAS) for 863 L4 Trojans and 380 L5 Trojans we derive the shape distribution for each of the clouds and find that, on average, the L4 asteroids are more elongated than the L5 asteroids. This shape difference is most likely due to the greater collision rate in the L4 cloud that results from its larger population. We additionally present the phase functions and c − o colours of 266 objects. Keywords: Jupiter trojans | multi-color photometry | sky surveys 1. INTRODUCTION Jupiter Trojans are minor planets that orbit 60 degrees ahead of (L4) and behind (L5) Jupiter in the 1:1 resonant Lagrange points. -
HUBBLE ULTRAVIOLET SPECTROSCOPY of JUPITER TROJANS Ian Wong1†, Michael E
Draft version March 11, 2019 Preprint typeset using LATEX style emulateapj v. 12/16/11 HUBBLE ULTRAVIOLET SPECTROSCOPY OF JUPITER TROJANS Ian Wong1y, Michael E. Brown2, Jordana Blacksberg3, Bethany L. Ehlmann2,3, and Ahmed Mahjoub3 1Department of Earth, Atmospheric, and Planetary Sciences, Massachusetts Institute of Technology, Cambridge, MA 02139, USA; [email protected] 2Division of Geological and Planetary Sciences, California Institute of Technology, Pasadena, CA 91125, USA 3Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA y51 Pegasi b Postdoctoral Fellow Draft version March 11, 2019 ABSTRACT We present the first ultraviolet spectra of Jupiter Trojans. These observations were carried out using the Space Telescope Imaging Spectrograph on the Hubble Space Telescope and cover the wavelength range 200{550 nm at low resolution. The targets include objects from both of the Trojan color sub- populations (less-red and red). We do not observe any discernible absorption features in these spectra. Comparisons of the averaged UV spectra of less-red and red targets show that the subpopulations are spectrally distinct in the UV. Less-red objects display a steep UV slope and a rollover at around 450 nm to a shallower visible slope, whereas red objects show the opposite trend. Laboratory spectra of irradiated ices with and without H2S exhibit distinct UV absorption features; consequently, the featureless spectra observed here suggest H2S alone is not responsible for the observed color bimodal- ity of Trojans, as has been previously hypothesized. We propose some possible explanations for the observed UV-visible spectra, including complex organics, space weathering of iron-bearing silicates, and masked features due to previous cometary activity. -
Astrocladistics of the Jovian Trojan Swarms
MNRAS 000,1–26 (2020) Preprint 23 March 2021 Compiled using MNRAS LATEX style file v3.0 Astrocladistics of the Jovian Trojan Swarms Timothy R. Holt,1,2¢ Jonathan Horner,1 David Nesvorný,2 Rachel King,1 Marcel Popescu,3 Brad D. Carter,1 and Christopher C. E. Tylor,1 1Centre for Astrophysics, University of Southern Queensland, Toowoomba, QLD, Australia 2Department of Space Studies, Southwest Research Institute, Boulder, CO. USA. 3Astronomical Institute of the Romanian Academy, Bucharest, Romania. Accepted XXX. Received YYY; in original form ZZZ ABSTRACT The Jovian Trojans are two swarms of small objects that share Jupiter’s orbit, clustered around the leading and trailing Lagrange points, L4 and L5. In this work, we investigate the Jovian Trojan population using the technique of astrocladistics, an adaptation of the ‘tree of life’ approach used in biology. We combine colour data from WISE, SDSS, Gaia DR2 and MOVIS surveys with knowledge of the physical and orbital characteristics of the Trojans, to generate a classification tree composed of clans with distinctive characteristics. We identify 48 clans, indicating groups of objects that possibly share a common origin. Amongst these are several that contain members of the known collisional families, though our work identifies subtleties in that classification that bear future investigation. Our clans are often broken into subclans, and most can be grouped into 10 superclans, reflecting the hierarchical nature of the population. Outcomes from this project include the identification of several high priority objects for additional observations and as well as providing context for the objects to be visited by the forthcoming Lucy mission. -
An Automated Search Procedure to Generate Optimal Low-Thrust Rendezvous Tours of the Sun-Jupiter Trojan Asteroids
AN AUTOMATED SEARCH PROCEDURE TO GENERATE OPTIMAL LOW-THRUST RENDEZVOUS TOURS OF THE SUN-JUPITER TROJAN ASTEROIDS Jeffrey R. Stuart(1) and Kathleen C. Howell(2) (1)Graduate Student, Purdue University, School of Aeronautics and Astronautics, 701 W. Stadium Ave., West Lafayette, IN, 47907, 765-620-4342, [email protected] (2)Hsu Lo Professor of Aeronautical and Astronautical Engineering, Purdue University, School of Aeronautics and Astronautics, 701 W. Stadium Ave., West Lafayette, IN, 47907, 765-494-5786, [email protected] Abstract: The Sun-Jupiter Trojan asteroid swarms are targets of interest for robotic spacecraft missions, and because of the relatively stable dynamics of the equilateral libration points, low-thrust propulsion systems offer a viable method for realizing tours of these asteroids. This investigation presents a novel scheme for the automated creation of prospective tours under the natural dynamics of the circular restricted three-body problem with thrust provided by a variable specific impulse low-thrust engine. The procedure approximates tours by combining independently generated fuel- optimal rendezvous arcs between pairs of asteroids into a series of coast periods near asteroids and engine operation durations between the asteroids. Propellant costs and departure and arrival times are estimated from performance of the individual thrust arcs. Tours of interest are readily re-converged in higher fidelity ephemeris models. In general, the automation procedure rapidly generates a large number of potential tours and supplies -
The Nordtvedt Effect in the Trojan Asteroids
View metadata, citation and similar papers at core.ac.uk brought to you by CORE provided by CERN Document Server (will be inserted by hand later) AND Your thesaurus codes are: ASTROPHYSICS 10(01.03.1; 01.05.1; 03.02.1; 07.37.1; 18.10.1) 5.7.2002 The Nordtvedt effect in the Trojan asteroids 1; 2; R.B. ORELLANA ∗ and H. VUCETICH ∗ 1 Observatorio Astron´omico de La Plata, Paseo del Bosque, (1900)La Plata, Argentina 2 Departamento de F´isica, Universidad Nacional de La PLata, C.C. 67, (1900)La Plata, Argentina Received October 5, accepted December 15, 1992 Abstract. Bounds to the Nordtvedt parameter are obtained from the motion of the first twelve Trojan asteroids in the period 1906-1990. From the analysis performed, we derive a value for the inverse of the Saturn mass 3497.80 0.81 and the Nordtvedt parameter ± -0.56 0.48, from a simultaneous solution for all asteroids. ± Key words: relativity - gravitation - asteroids - astronomical constants - celestial me- chanics 1. Introduction The asteroids located in the vicinity of the equilateral triangle solutions of Lagrange (L4 and L5), known as the Trojan asteroids, are particularly sensitive to a possible viola- tion of the Principle of Equivalence (Nordtvedt, 1968) because they act as a resonator selecting long period perturbations. Theories of gravitation alternatives to General Rel- ativity predict a difference between inertial (mi ) and passive gravitational (mg ) masses of a planetary-sized body (the so-called Nordtvedt effect) equal to: m g =1+∆; (1) mi For the sun, the correction term ∆ is equal to: 15GM ∆ = η, (2) 2R c2 ?Member of C.O.N.I.C.E.T. -
The Minor Planet Bulletin
THE MINOR PLANET BULLETIN OF THE MINOR PLANETS SECTION OF THE BULLETIN ASSOCIATION OF LUNAR AND PLANETARY OBSERVERS VOLUME 38, NUMBER 2, A.D. 2011 APRIL-JUNE 71. LIGHTCURVES OF 10452 ZUEV, (14657) 1998 YU27, AND (15700) 1987 QD Gary A. Vander Haagen Stonegate Observatory, 825 Stonegate Road Ann Arbor, MI 48103 [email protected] (Received: 28 October) Lightcurve observations and analysis revealed the following periods and amplitudes for three asteroids: 10452 Zuev, 9.724 ± 0.002 h, 0.38 ± 0.03 mag; (14657) 1998 YU27, 15.43 ± 0.03 h, 0.21 ± 0.05 mag; and (15700) 1987 QD, 9.71 ± 0.02 h, 0.16 ± 0.05 mag. Photometric data of three asteroids were collected using a 0.43- meter PlaneWave f/6.8 corrected Dall-Kirkham astrograph, a SBIG ST-10XME camera, and V-filter at Stonegate Observatory. The camera was binned 2x2 with a resulting image scale of 0.95 arc- seconds per pixel. Image exposures were 120 seconds at –15C. Candidates for analysis were selected using the MPO2011 Asteroid Viewing Guide and all photometric data were obtained and analyzed using MPO Canopus (Bdw Publishing, 2010). Published asteroid lightcurve data were reviewed in the Asteroid Lightcurve Database (LCDB; Warner et al., 2009). The magnitudes in the plots (Y-axis) are not sky (catalog) values but differentials from the average sky magnitude of the set of comparisons. The value in the Y-axis label, “alpha”, is the solar phase angle at the time of the first set of observations. All data were corrected to this phase angle using G = 0.15, unless otherwise stated. -
Appendix 1 1311 Discoverers in Alphabetical Order
Appendix 1 1311 Discoverers in Alphabetical Order Abe, H. 28 (8) 1993-1999 Bernstein, G. 1 1998 Abe, M. 1 (1) 1994 Bettelheim, E. 1 (1) 2000 Abraham, M. 3 (3) 1999 Bickel, W. 443 1995-2010 Aikman, G. C. L. 4 1994-1998 Biggs, J. 1 2001 Akiyama, M. 16 (10) 1989-1999 Bigourdan, G. 1 1894 Albitskij, V. A. 10 1923-1925 Billings, G. W. 6 1999 Aldering, G. 4 1982 Binzel, R. P. 3 1987-1990 Alikoski, H. 13 1938-1953 Birkle, K. 8 (8) 1989-1993 Allen, E. J. 1 2004 Birtwhistle, P. 56 2003-2009 Allen, L. 2 2004 Blasco, M. 5 (1) 1996-2000 Alu, J. 24 (13) 1987-1993 Block, A. 1 2000 Amburgey, L. L. 2 1997-2000 Boattini, A. 237 (224) 1977-2006 Andrews, A. D. 1 1965 Boehnhardt, H. 1 (1) 1993 Antal, M. 17 1971-1988 Boeker, A. 1 (1) 2002 Antolini, P. 4 (3) 1994-1996 Boeuf, M. 12 1998-2000 Antonini, P. 35 1997-1999 Boffin, H. M. J. 10 (2) 1999-2001 Aoki, M. 2 1996-1997 Bohrmann, A. 9 1936-1938 Apitzsch, R. 43 2004-2009 Boles, T. 1 2002 Arai, M. 45 (45) 1988-1991 Bonomi, R. 1 (1) 1995 Araki, H. 2 (2) 1994 Borgman, D. 1 (1) 2004 Arend, S. 51 1929-1961 B¨orngen, F. 535 (231) 1961-1995 Armstrong, C. 1 (1) 1997 Borrelly, A. 19 1866-1894 Armstrong, M. 2 (1) 1997-1998 Bourban, G. 1 (1) 2005 Asami, A. 7 1997-1999 Bourgeois, P. 1 1929 Asher, D. -
Trojan Tour Decadal Study
SDO-12348 Trojan Tour Decadal Study Mike Brown [email protected] SDO-12348 Planetary Science Decadal Survey Mission Concept Study Final Report Executive Summary ................................................................................................................ 5 1. Scientific Objectives ......................................................................................................... 6 Science Questions and Objectives ................................................................................................................................... 6 Science Traceability ............................................................................................................................................................ 12 2. High‐Level Mission Concept ........................................................................................... 14 Study Request and Concept Maturity Level .............................................................................................................. 14 Overview ................................................................................................................................................................................. 14 Technology Maturity .......................................................................................................................................................... 16 Key Trades ............................................................................................................................................................................. -
Updated on 1 September 2018
20813 Aakashshah 12608 Aesop 17225 Alanschorn 266 Aline 31901 Amitscheer 30788 Angekauffmann 2341 Aoluta 23325 Arroyo 15838 Auclair 24649 Balaklava 26557 Aakritijain 446 Aeternitas 20341 Alanstack 8651 Alineraynal 39678 Ammannito 11911 Angel 19701 Aomori 33179 Arsenewenger 9117 Aude 16116 Balakrishnan 28698 Aakshi 132 Aethra 21330 Alanwhitman 214136 Alinghi 871 Amneris 28822 Angelabarker 3810 Aoraki 29995 Arshavsky 184535 Audouze 3749 Balam 28828 Aalamiharandi 1064 Aethusa 2500 Alascattalo 108140 Alir 2437 Amnestia 129151 Angelaboggs 4094 Aoshima 404 Arsinoe 4238 Audrey 27381 Balasingam 33181 Aalokpatwa 1142 Aetolia 19148 Alaska 14225 Alisahamilton 32062 Amolpunjabi 274137 Angelaglinos 3400 Aotearoa 7212 Artaxerxes 31677 Audreyglende 20821 Balasridhar 677 Aaltje 22993 Aferrari 200069 Alastor 2526 Alisary 1221 Amor 16132 Angelakim 9886 Aoyagi 113951 Artdavidsen 20004 Audrey-Lucienne 26634 Balasubramanian 2676 Aarhus 15467 Aflorsch 702 Alauda 27091 Alisonbick 58214 Amorim 30031 Angelakong 11258 Aoyama 44455 Artdula 14252 Audreymeyer 2242 Balaton 129100 Aaronammons 1187 Afra 5576 Albanese 7517 Alisondoane 8721 AMOS 22064 Angelalewis 18639 Aoyunzhiyuanzhe 1956 Artek 133007 Audreysimmons 9289 Balau 22656 Aaronburrows 1193 Africa 111468 Alba Regia 21558 Alisonliu 2948 Amosov 9428 Angelalouise 90022 Apache Point 11010 Artemieva 75564 Audubon 214081 Balavoine 25677 Aaronenten 6391 Africano 31468 Albastaki 16023 Alisonyee 198 Ampella 25402 Angelanorse 134130 Apaczai 105 Artemis 9908 Aue 114991 Balazs 11451 Aarongolden 3326 Agafonikov 10051 Albee -
Appendix 1 897 Discoverers in Alphabetical Order
Appendix 1 897 Discoverers in Alphabetical Order Abe, H. 22 (7) 1993-1999 Bohrmann, A. 9 1936-1938 Abraham, M. 3 (3) 1999 Bonomi, R. 1 (1) 1995 Aikman, G. C. L. 3 1994-1997 B¨orngen, F. 437 (161) 1961-1995 Akiyama, M. 14 (10) 1989-1999 Borrelly, A. 19 1866-1894 Albitskij, V. A. 10 1923-1925 Bourgeois, P. 1 1929 Aldering, G. 3 1982 Bowell, E. 563 (6) 1977-1994 Alikoski, H. 13 1938-1953 Boyer, L. 40 1930-1952 Alu, J. 20 (11) 1987-1993 Brady, J. L. 1 1952 Amburgey, L. L. 1 1997 Brady, N. 1 2000 Andrews, A. D. 1 1965 Brady, S. 1 1999 Antal, M. 17 1971-1988 Brandeker, A. 1 2000 Antonini, P. 25 (1) 1996-1999 Brcic, V. 2 (2) 1995 Aoki, M. 1 1996 Broughton, J. 179 1997-2002 Arai, M. 43 (43) 1988-1991 Brown, J. A. 1 (1) 1990 Arend, S. 51 1929-1961 Brown, M. E. 1 (1) 2002 Armstrong, C. 1 (1) 1997 Broˇzek, L. 23 1979-1982 Armstrong, M. 2 (1) 1997-1998 Bruton, J. 1 1997 Asami, A. 5 1997-1999 Bruton, W. D. 2 (2) 1999-2000 Asher, D. J. 9 1994-1995 Bruwer, J. A. 4 1953-1970 Augustesen, K. 26 (26) 1982-1987 Buchar, E. 1 1925 Buie, M. W. 13 (1) 1997-2001 Baade, W. 10 1920-1949 Buil, C. 4 1997 Babiakov´a, U. 4 (4) 1998-2000 Burleigh, M. R. 1 (1) 1998 Bailey, S. I. 1 1902 Burnasheva, B. A. 13 1969-1971 Balam, D.