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Tides and the Climate: Some Speculations
FEBRUARY 2007 MUNK AND BILLS 135 Tides and the Climate: Some Speculations WALTER MUNK Scripps Institution of Oceanography, La Jolla, California BRUCE BILLS Scripps Institution of Oceanography, La Jolla, California, and NASA Goddard Space Flight Center, Greenbelt, Maryland (Manuscript received 18 May 2005, in final form 12 January 2006) ABSTRACT The important role of tides in the mixing of the pelagic oceans has been established by recent experiments and analyses. The tide potential is modulated by long-period orbital modulations. Previously, Loder and Garrett found evidence for the 18.6-yr lunar nodal cycle in the sea surface temperatures of shallow seas. In this paper, the possible role of the 41 000-yr variation of the obliquity of the ecliptic is considered. The obliquity modulation of tidal mixing by a few percent and the associated modulation in the meridional overturning circulation (MOC) may play a role comparable to the obliquity modulation of the incoming solar radiation (insolation), a cornerstone of the Milankovic´ theory of ice ages. This speculation involves even more than the usual number of uncertainties found in climate speculations. 1. Introduction et al. 2000). The Hawaii Ocean-Mixing Experiment (HOME), a major experiment along the Hawaiian Is- An early association of tides and climate was based land chain dedicated to tidal mixing, confirmed an en- on energetics. Cold, dense water formed in the North hanced mixing at spring tides and quantified the scat- Atlantic would fill up the global oceans in a few thou- tering of tidal energy from barotropic into baroclinic sand years were it not for downward mixing from the modes over suitable topography. -
Geological Constraints on the Precambrian History of Earth's
GEOLOGICAL CONSTRAINTS ON THE PRECAMBRIAN HISTORY OF EARTH’S ROTATION AND THE MOON’S ORBIT George E. Williams Department of Geology and Geophysics University of Adelaide, Adelaide South Australia, Australia Abstract. Over the past decade the analysis of sedi- zoic (ϳ620 Ma) tidal rhythmites in South Australia are mentary cyclic rhythmites of tidal origin, i.e., stacked validated by these tests and indicate 13.1 Ϯ 0.1 synodic thin beds or laminae usually of sandstone, siltstone, and (lunar) months/yr, 400 Ϯ 7 solar days/yr, a length of day Ϯ mudstone that display periodic variations in thickness of 21.9 0.4 h, and a relative Earth-Moon distance a/a0 reflecting a strong tidal influence on sedimentation, has of 0.965 Ϯ 0.005. The mean rate of lunar recession since provided information on Earth’s paleorotation and the that time is 2.17 Ϯ 0.31 cm/yr, which is little more than evolving lunar orbit for Precambrian time (before 540 half the present rate of lunar recession of 3.82 Ϯ 0.07 Ma). Depositional environments of tidal rhythmites cm/yr obtained by lunar laser ranging. The late Neopro- range from estuarine to tidal delta, with a wave-pro- terozoic data militate against significant overall change tected, distal ebb tidal delta setting being particularly in Earth’s moment of inertia and radius at least since 620 favorable for the deposition and preservation of long, Ma. Cyclicity displayed by Paleoproterozoic (2450 Ma) detailed rhythmite records. The potential sediment load banded iron formation in Western Australia may record of nearshore tidal currents and the effectiveness of the tidal influences on the discharge and/or dispersal of tide as an agent of sediment entrainment and deposition submarine hydrothermal plumes and suggests 14.5 Ϯ 0.5 ϭ Ϯ are related directly to tidal range (or maximum tidal synodic months/yr and a/a0 0.906 0.029. -
Space Weapons Earth Wars
CHILDREN AND FAMILIES The RAND Corporation is a nonprofit institution that EDUCATION AND THE ARTS helps improve policy and decisionmaking through ENERGY AND ENVIRONMENT research and analysis. HEALTH AND HEALTH CARE This electronic document was made available from INFRASTRUCTURE AND www.rand.org as a public service of the RAND TRANSPORTATION Corporation. INTERNATIONAL AFFAIRS LAW AND BUSINESS NATIONAL SECURITY Skip all front matter: Jump to Page 16 POPULATION AND AGING PUBLIC SAFETY SCIENCE AND TECHNOLOGY Support RAND Purchase this document TERRORISM AND HOMELAND SECURITY Browse Reports & Bookstore Make a charitable contribution For More Information Visit RAND at www.rand.org Explore RAND Project AIR FORCE View document details Limited Electronic Distribution Rights This document and trademark(s) contained herein are protected by law as indicated in a notice appearing later in this work. This electronic representation of RAND intellectual property is provided for non-commercial use only. Unauthorized posting of RAND electronic documents to a non-RAND website is prohibited. RAND electronic documents are protected under copyright law. Permission is required from RAND to reproduce, or reuse in another form, any of our research documents for commercial use. For information on reprint and linking permissions, please see RAND Permissions. The monograph/report was a product of the RAND Corporation from 1993 to 2003. RAND monograph/reports presented major research findings that addressed the challenges facing the public and private sectors. They included executive summaries, technical documentation, and synthesis pieces. SpaceSpace WeaponsWeapons EarthEarth WarsWars Bob Preston | Dana J. Johnson | Sean J.A. Edwards Michael Miller | Calvin Shipbaugh Project AIR FORCE R Prepared for the United States Air Force Approved for public release; distribution unlimited The research reported here was sponsored by the United States Air Force under Contract F49642-01-C-0003. -
An Adaptive Groundtrack Maintenance Scheme For
An Adaptive Groundtrack Maintenance Scheme for Spacecraft with Electric Propulsion Mirko Leomanni1, Andrea Garulli, Antonio Giannitrapani Dipartimento di Ingegneria dell’Informazione e Scienze Matematiche Universit`adi Siena, Siena, Italy Fabrizio Scortecci Aerospazio Tenologie Rapolano Terme, Siena, Italy Abstract In this paper, the repeat-groundtrack orbit maintenance problem is addressed for spacecraft driven by electric propulsion. An adaptive solution is proposed, which combines an hysteresis controller and a recursive least squares filter. The controller provides a pulse-width modulated command to the thruster, in com- pliance with the peculiarities of the electric propulsion technology. The filter takes care of estimating a set of environmental disturbance parameters, from inertial position and velocity measurements. The resulting control scheme is able to compensate for the groundtrack drift due to atmospheric drag, in a fully autonomous manner. A numerical study of a low Earth orbit mission confirms the effectiveness of the proposed method. Keywords: Ground Track Maintenance, Electric Propulsion, Low Earth Orbit 1. Introduction arXiv:1807.08109v2 [cs.SY] 3 Jun 2019 Recent years have seen a growing trend in the development of Low Earth Orbit (LEO) space missions for commercial, strategic, and scientific purposes. Examples include Earth Observation programs such as DMC, RapidEye and Pl´eiades-Neo [1, 2], as well as broadband constellations like OneWeb, Starlink Email addresses: [email protected] (Mirko Leomanni), [email protected] (Andrea Garulli), [email protected] (Antonio Giannitrapani), [email protected] (Fabrizio Scortecci) 1Corresponding author Preprint submitted to Elsevier June 4, 2019 and Telesat [3]. As opposed to geostationary spacecraft, a LEO satellite can- not stay always pointed towards a fixed spot on Earth. -
Perturbations of Circular Synchronous Satellite
PERTURBATIONS OF CIRCULAR SYNCHRONOUS SATELLITE ORBITS Richard L. Dunn 5 February 1962 8616-600 5-RU-000 Prepared by Ridhard L. Dunn Project Engineer Systems Analysis Department Approved by 6, ;V. T+ R. M. Page 'y Manager Systems Analysis Department Approved by Director Com m uni cation Laborat o r y SPACE TECHNOLOGY LABORATORIES, INC. A Subsidiary of Thompson Ram0 Wooldridge, Inc. One Space Park - Redondo Beach, California Page ii ABSTRACT Satellite drift maxima from a synchronous inclined circular orbit due to perturbations are investigated. A syn- chronous satellite, one which retraces its ground track eacb day, will tend to drift from the initially synchronous trajectory in time. Six, twelve, and twenty-four hour period orbits receive special attention. Page iii CONTENTS Page I. INTRODUCTION .................... 1 11. THE NODAL PERIOD ................. 1 111. ORBITAL INCLINATION ............... 4 IV. TIMEDRIFT. ..................... 7 V. MISS IN TRUE ANOMALY. .............. 8 VI. DRIFT IN LATITUDE ................. 11 VI1 SUMMARY. ...................... 12 Page 1 I. INTRQDUCTIGN A constant ground track or synchronous satellite is one which ideally retraces its ground track each day. Assume that the satellite is initially over some fixed point A on the earth's surface. Assume also that this occurs at the ascending node. When the satellite reaches its node about one day later, Point A will again be there. As time goes on the satellite will tend to arrive early or late and thus miss passing over Point A. Assuming perfect guidance this miss is mainly caused by lunar and solar forces exerted on the orbit. The miss can be expressed by the angle AV between the radius vectors to Point A and to the satellite at the time Point A and the projection upon the earth of the orbits ascending node coincide. -
Professor S Afanasiev's Nanocycles Method
Cycles Research Institute June 2005 and new moon for solar eclipses. But it does not Professor S Afanasiev's happen every full and new moon, because Nanocycles Method sometimes the moon passes above or below the direct line between the sun and earth. When by Ray Tomes either node of the moon's orbit is at or near the direction between the earth and sun then it is Russian translation by Michael Taler possible to have eclipses. A new method of dating geological deposits has Eclipses are not important in the nanocycles been devised by Professor S Afanasiev and method, however at the same time as eclipses described in his 1991 book “Nanocycles Method”. occur, the tidal pull of the sun and moon are The book is in Russian which the author cannot fully combined to make the very strongest tides. read, but with text translation help from Michael At other times the moon may pass up to 5 Taler, the tables largely explain themselves to degrees above or below the line connecting the someone who knows about the moons orbital earth and sun and the tidal range is not so parameters. extreme. These spring tides as they are often called can happen at any time of the year and at This article is not intended to be a complete present come at an interval of a little under 6 translation or review of the book, but only to months. deal with matters relating to the dating of geological deposits. There is considerable extra There are other factors that affect the strength of material in the book, although this may be seen tides also, such as whether the moon is at its as the central theme. -
Chaos in Navigation Satellite Orbits Caused by the Perturbed Motion Of
Mon. Not. R. Astron. Soc. 000, 1–6 (2015) Printed 10 March 2015 (MN LATEX style file v2.2) Chaos in navigation satellite orbits caused by the perturbed motion of the Moon Aaron J. Rosengren,1⋆ Elisa Maria Alessi,1 Alessandro Rossi1 and Giovanni B. Valsecchi1,2 1IFAC-CNR, Via Madonna del Piano 10, 50019 Sesto Fiorentino (FI), Italy 2IAPS-INAF, Via Fosso del Cavaliere 100, 00133 Roma, Italy ABSTRACT Numerical simulations carried out over the past decade suggest that the orbits of the Global Navigation Satellite Systems are unstable, resulting in an apparent chaotic growth of the ec- centricity. Here we show that the irregular and haphazard character of these orbits reflects a similar irregularity in the orbits of many celestial bodies in our Solar System. We find that secular resonances, involving linear combinations of the frequencies of nodal and apsidal pre- cession and the rate of regression of lunar nodes, occur in profusion so that the phase space is threaded by a devious stochastic web. As in all cases in the Solar System, chaos ensues where resonances overlap. These results may be significant for the analysis of disposal strategies for the four constellations in this precarious region of space. Key words: celestial mechanics – chaos – methods: analytical – methods: numerical – planets and satellites: dynamical evolution and stability — planets and satellites: general. 1 INTRODUCTION behaviour. To identify the source of orbital instability, we inves- tigated the main resonant structures that organise and govern the Space debris—remnants of past missions, satellite explosions, and long-term orbital motion of navigation satellites. This paper clari- collisions—is a phenomenon that has existed since the beginning of fies the fundamental role played by secular resonances and reveals the space age; however, its significance for space activities, in par- the significance of the perturbed motion of the Moon. -
Exploring the Relationship Between Outer Space and World Politics: English School and Regime Theory Perspectives
Exploring the Relationship Between Outer Space and World Politics: English School and Regime Theory Perspectives Jill Stuart A thesis submitted to the Department of International Relations of the London School of Economics and Political Science for the degree of Doctor of Philosophy in International Relations UMI Number: U615931 All rights reserved INFORMATION TO ALL USERS The quality of this reproduction is dependent upon the quality of the copy submitted. In the unlikely event that the author did not send a complete manuscript and there are missing pages, these will be noted. Also, if material had to be removed, a note will indicate the deletion. Dissertation Publishing UMI U615931 Published by ProQuest LLC 2014. Copyright in the Dissertation held by the Author. Microform Edition © ProQuest LLC. All rights reserved. This work is protected against unauthorized copying under Title 17, United States Code. ProQuest LLC 789 East Eisenhower Parkway P.O. Box 1346 Ann Arbor, Ml 48106-1346 Author Declaration I certify that the thesis I have presented for examination for the MPhil/PhD degree of the London School of Economics and Political Science is solely my own work other than where I have clearly indicated that it is the work of others (in which case the extent of any work carried out jointly by me and any other person is clearly identified in it). The copyright of this thesis rests with the author. Quotation from it is permitted, provided that full acknowledgement is made. This thesis may not be reproduced without the prior written consent of the author. I warrant that this authorization does not, to the best of my belief, infringe the rights of any third party. -
The Design and Simulation of an Astronomical Clock
applied sciences Article The Design and Simulation of an Astronomical Clock Branislav Popkonstantinovi´c 1,*, Ratko Obradovi´c 2 , Miša Stoji´cevi´c 1 , Zorana Jeli 1, Ivana Cvetkovi´c 1, Ivana Vasiljevi´c 2 and Zoran Milojevi´c 3,* 1 Faculty of Mechanical Engineering, University of Belgrade, 11000 Belgrade, Serbia; [email protected] (M.S.); [email protected] (Z.J.); [email protected] (I.C.) 2 Faculty of Technical Sciences, University of Novi Sad, 21000 Novi Sad, Serbia; [email protected] (R.O.); [email protected] (I.V.) 3 School of Engineering, Newcastle University, Newcastle upon Tyne NE1 7RU, UK * Correspondence: [email protected] (B.P.); [email protected] (Z.M.) Abstract: This paper describes and explains the synthesis of an astronomical clock mechanism which displays the mean position of the Sun, the Moon, the lunar node and zodiac circle as well as the Moon phases and their motion during the year as seen from the Earth. The clock face represents the stereographic projection of the celestial equator, celestial tropics, zodiac circle (ecliptic) and horizon for the latitude of Belgrade from the north celestial pole to the equator plane. The observed motions of celestial objects are realized by a set of clock gear trains with properly calculated gear ratios. The method of continued fraction is applied in the computation of proper and practically applicable gear ratios of the clock gear trains. The fully operational 3D model of the astronomical clock is created and the motion study of its operation is accomplished by using the SolidWorks 2016 application. -
Tidal Rhythmites and Their Implications
Earth-Science Reviews 69 (2005) 79–95 www.elsevier.com/locate/earscirev Tidal rhythmites and their implications Rajat Mazumder*, Makoto Arima Geological Institute, Graduate School of Environment and Information Sciences, Yokohama National University, 79-7, Tokiwadai, Hodogaya, Yokohama 240 8501, Japan Received 22 March 2004; accepted 7 July 2004 Abstract Tidal rhythmites are unequivocal evidence of marine conditions in sedimentary basins and can preserve a record of astronomically induced tidal periods. Unlike modern tide and tidal deposits, analysis of ancient tidal rhythmites, however, is not straightforward. This paper highlights the advances made in the tidal rhythmite research in the last decade and reviews the methodologies of extracting lunar orbital periods from ancient tidal rhythmites, the mathematics behind the use of tidalites, and their limitations and uncertainties. We have shown that analysis of ancient tidal rhythmite may help us to estimate the palaeolunar orbital periods in terms of lunar days/month accurately. Determination of absolute Earth–Moon distances and Earth’s palaeorotational parameters in the distant geological past from tidal rhythmite, however, is ambiguous because of the difficulties in determining the absolute length of the ancient lunar sidereal month. D 2004 Elsevier B.V. All rights reserved. Keywords: Tidal rhythmites; Lunar orbital period; Earth–Moon distance; Palaeogeophysics; Universal gravitational constant 1. Introduction evidence of marine conditions in sedimentary basins (cf. Eriksson et al., 1998; Eriksson and Simpson, 2004). Tidal rhythmites are packages of laterally and/or Tidal rhythmites have been used to interpret palae- vertically accreted, laminated to thinly bedded oclimate (Kvale et al., 1994; Miller and Eriksson, medium- to fine-grained sandstone, siltstone and 1997) and palaeo-ocean seiches (Archer, 1996a). -
Section 2. Satellite Orbits
Section 2. Satellite Orbits References • Kidder and Vonder Haar: chapter 2 • Stephens: chapter 1, pp. 25-30 • Rees: chapter 9, pp. 174-192 In order to understand satellites and the remote sounding data obtained by instruments located on satellites, we need to know something about orbital mechanics, especially the orbits in which satellites are constrained to move and the geometry with which they view the Earth. 2.1 Orbital Mechanics The use of satellites as platforms for remote sounding is based on some very fundamental physics. Newton's Laws of Motion and Gravitation (1686) → the basis for classical mechanics Laws of motion: (1) Every body continues in its state of rest or of uniform motion in a straight line unless it is compelled to change that state by a force impressed upon it. (2) The rate of change of momentum is proportional to the impressed force and is in the same direction as that force. d(mv) dv Momentum = mass × velocity, so Law (2) becomes F = = m = a dt dt for constant mass (3) For every action, there is an equal and opposite reaction. Law of gravitation: The force of attraction between any two particles is • proportional to their masses • inversely proportional to the square of the distance between them Gm m i.e. F = 1 2 (treating the masses as points) r 2 where G = gravitational constant = 6.673 × 10-11 Nm2/kg2 ___________________________________________________________________________________ PHY 499S – Earth Observations from Space, Spring Term 2005 (K. Strong) page 2-1 These laws explain how a satellite stays in orbit. Law (1): A satellite would tend to go off in a straight line if no force were applied to it. -
Summer Study on Post-Apollo Lunar Science
POST-APOLLO LUNAR SC IENCE Report of a Study by the Lunar Science Institute July 1972 Lunar Science Institute 3303 NASA Road 1 Houston, Texas 77058 Copyright @ 1972 by the Lunar Science Institute Library of Congress Catalog Card No. 72-93379 SUMMER STUDY ON POST-APOLLO LUNAR SCIENCE J. W. Chamberlain, Director Eugene M. Shoemaker Lunar Science Institute California Institute of Technology R. A. Phinney (Chairman) Princeton University Nafi M. Toksoz Massachusetts Institute John B. Adams (Co-Chairman) of Techno Zogy Fairleigh Dickinson University Robert M. Walker Washington University P. J. Coleman (Co-Chairman) University of California Gerald J. Wasserburg Los Angeles C~ZiforniaInstitute of Techno Zogy E. Anders A. L. Burlingame Enrioo Fermi Institute University of CaZifornia Berkeley Kinsey A. Anderson University of California J. Cone1 Berkeley Jet PropuZsion Laboratory James R. Arnold D. R. Criswell University of California Lunar Science Institute San ~ie~o- Michael B. Duke G. Arrhenius NASA/MSC University of California San Diego Geoffrey Eglinton University of BristoZ Ralph R. Baker Colorado State University Farouk El-Baz Bet Zcomm, Inc. .Peter M. Bell Carnegie Institution Michael Fuller of Washington university of Pittsburgh Roy G. Brereton Paul Gast Jet P~opulsionLaboratory NASA/MSC Robin P. Brett H. Taylor Howard NASA/MSC Stanford University iii W. M. Kaula S. K. Runcorn University of California University of NewcastZe Los AngeZes upon Tyne Robert L. Kovach Roman A. Schmitt Stanford University Oregon State University Gary Latham Leon T. Silver Marine BiomedicaZ Institute CaZifornia Institute University of Texas of Techno Zogy Kurt Marti W. L. Sjogren University of Ca Zifornia Jet PropuZsion Laboratory Sun Diego Charles P.