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Captain Vancouver, Longitude Errors, 1792
Context: Captain Vancouver, longitude errors, 1792 Citation: Doe N.A., Captain Vancouver’s longitudes, 1792, Journal of Navigation, 48(3), pp.374-5, September 1995. Copyright restrictions: Please refer to Journal of Navigation for reproduction permission. Errors and omissions: None. Later references: None. Date posted: September 28, 2008. Author: Nick Doe, 1787 El Verano Drive, Gabriola, BC, Canada V0R 1X6 Phone: 250-247-7858, FAX: 250-247-7859 E-mail: [email protected] Captain Vancouver's Longitudes – 1792 Nicholas A. Doe (White Rock, B.C., Canada) 1. Introduction. Captain George Vancouver's survey of the North Pacific coast of America has been characterized as being among the most distinguished work of its kind ever done. For three summers, he and his men worked from dawn to dusk, exploring the many inlets of the coastal mountains, any one of which, according to the theoretical geographers of the time, might have provided a long-sought-for passage to the Atlantic Ocean. Vancouver returned to England in poor health,1 but with the help of his brother John, he managed to complete his charts and most of the book describing his voyage before he died in 1798.2 He was not popular with the British Establishment, and after his death, all of his notes and personal papers were lost, as were the logs and journals of several of his officers. Vancouver's voyage came at an interesting time of transition in the technology for determining longitude at sea.3 Even though he had died sixteen years earlier, John Harrison's long struggle to convince the Board of Longitude that marine chronometers were the answer was not quite over. -
Librational Response of Europa, Ganymede, and Callisto with an Ocean for a Non-Keplerian Orbit
A&A 527, A118 (2011) Astronomy DOI: 10.1051/0004-6361/201015304 & c ESO 2011 Astrophysics Librational response of Europa, Ganymede, and Callisto with an ocean for a non-Keplerian orbit N. Rambaux1,2, T. Van Hoolst3, and Ö. Karatekin3 1 Université Pierre et Marie Curie, Paris VI, IMCCE, Observatoire de Paris, 77 avenue Denfert-Rochereau, 75014 Paris, France 2 IMCCE, Observatoire de Paris, CNRS UMR 8028, 77 avenue Denfert-Rochereau, 75014 Paris, France e-mail: [email protected] 3 Royal Observatory of Belgium, 3 avenue Circulaire, 1180 Brussels, Belgium e-mail: [tim.vanhoolst;ozgur.karatekin]@oma.be Received 30 June 2010 / Accepted 8 September 2010 ABSTRACT Context. The Galilean satellites Europa, Ganymede, and Callisto are thought to harbor a subsurface ocean beneath an ice shell but its properties, such as the depth beneath the surface, have not been well constrained. Future geodetic observations with, for example, space missions like the Europa Jupiter System Mission (EJSM) of NASA and ESA may refine our knowledge about the shell and ocean. Aims. Measurement of librational motion is a useful tool for detecting an ocean and characterizing the interior parameters of the moons. The objective of this paper is to investigate the librational response of Galilean satellites, Europa, Ganymede, and Callisto assumed to have a subsurface ocean by taking the perturbations of the Keplerian orbit into account. Perturbations from a purely Keplerian orbit are caused by gravitational attraction of the other Galilean satellites, the Sun, and the oblateness of Jupiter. Methods. We use the librational equations developed for a satellite with a subsurface ocean in synchronous spin-orbit resonance. -
Equation of Time — Problem in Astronomy M
This paper was awarded in the II International Competition (1993/94) "First Step to Nobel Prize in Physics" and published in the competition proceedings (Acta Phys. Pol. A 88 Supplement, S-49 (1995)). The paper is reproduced here due to kind agreement of the Editorial Board of "Acta Physica Polonica A". EQUATION OF TIME | PROBLEM IN ASTRONOMY M. Muller¨ Gymnasium M¨unchenstein, Grellingerstrasse 5, 4142 M¨unchenstein, Switzerland Abstract The apparent solar motion is not uniform and the length of a solar day is not constant throughout a year. The difference between apparent solar time and mean (regular) solar time is called the equation of time. Two well-known features of our solar system lie at the basis of the periodic irregularities in the solar motion. The angular velocity of the earth relative to the sun varies periodically in the course of a year. The plane of the orbit of the earth is inclined with respect to the equatorial plane. Therefore, the angular velocity of the relative motion has to be projected from the ecliptic onto the equatorial plane before incorporating it into the measurement of time. The math- ematical expression of the projection factor for ecliptic angular velocities yields an oscillating function with two periods per year. The difference between the extreme values of the equation of time is about half an hour. The response of the equation of time to a variation of its key parameters is analyzed. In order to visualize factors contributing to the equation of time a model has been constructed which accounts for the elliptical orbit of the earth, the periodically changing angular velocity, and the inclined axis of the earth. -
Synopsis of Euler's Paper E105
1 Synopsis of Euler’s paper E105 -- Memoire sur la plus grande equation des planetes (Memoir on the Maximum value of an Equation of the Planets) Compiled by Thomas J Osler and Jasen Andrew Scaramazza Mathematics Department Rowan University Glassboro, NJ 08028 [email protected] Preface The following summary of E 105 was constructed by abbreviating the collection of Notes. Thus, there is considerable repetition in these two items. We hope that the reader can profit by reading this synopsis before tackling Euler’s paper itself. I. Planetary Motion as viewed from the earth vs the sun ` Euler discusses the fact that planets observed from the earth exhibit a very irregular motion. In general, they move from west to east along the ecliptic. At times however, the motion slows to a stop and the planet even appears to reverse direction and move from east to west. We call this retrograde motion. After some time the planet stops again and resumes its west to east journey. However, if we observe the planet from the stand point of an observer on the sun, this retrograde motion will not occur, and only a west to east path of the planet is seen. II. The aphelion and the perihelion From the sun, (point O in figure 1) the planet (point P ) is seen to move on an elliptical orbit with the sun at one focus. When the planet is farthest from the sun, we say it is at the “aphelion” (point A ), and at the perihelion when it is closest. The time for the planet to move from aphelion to perihelion and back is called the period. -
Absolute and Relative Motion Satellite Theories for Zonal and Tesseral Gravitational Harmonics
ABSOLUTE AND RELATIVE MOTION SATELLITE THEORIES FOR ZONAL AND TESSERAL GRAVITATIONAL HARMONICS A Dissertation by BHARAT MAHAJAN Submitted to the Office of Graduate and Professional Studies of Texas A&M University in partial fulfillment of the requirements for the degree of DOCTOR OF PHILOSOPHY Chair of Committee, Srinivas R. Vadali Co-Chair of Committee, Kyle T. Alfriend Committee Members, John E. Hurtado Igor Zelenko Head of Department, Rodney Browersox May 2018 Major Subject: Aerospace Engineering Copyright 2018 Bharat Mahajan ABSTRACT In 1959, Dirk Brouwer pioneered the use of the Hamiltonian perturbation methods for con- structing artificial satellite theories with effects due to nonspherical gravitational perturbations in- cluded. His solution specifically accounted for the effects of the first few zonal spherical harmon- ics. However, the development of a closed-form (in the eccentricity) satellite theory that accounts for any arbitrary spherical harmonic perturbation remains a challenge to this day. In the present work, the author has obtained novel solutions for the absolute and relative motion of artificial satel- lites (absolute motion in this work refers to the motion relative to the central gravitational body) for an arbitrary zonal or tesseral spherical harmonic by using Hamiltonian perturbation methods, without resorting to expansions in either the eccentricity or the small ratio of the satellite’s mean motion and the angular velocity of the central body. First, generalized closed-form expressions for the secular, long-period, and short-period variations of the equinoctial orbital elements due to an arbitrary zonal harmonic are derived, along with the explicit expressions for the first six zonal harmonics. -
NOAA Technical Memorandum ERL ARL-94
NOAA Technical Memorandum ERL ARL-94 THE NOAA SOLAR EPHEMERIS PROGRAM Albion D. Taylor Air Resources Laboratories Silver Spring, Maryland January 1981 NOAA 'Technical Memorandum ERL ARL-94 THE NOAA SOLAR EPHEMERlS PROGRAM Albion D. Taylor Air Resources Laboratories Silver Spring, Maryland January 1981 NOTICE The Environmental Research Laboratories do not approve, recommend, or endorse any proprietary product or proprietary material mentioned in this publication. No reference shall be made to the Environmental Research Laboratories or to this publication furnished by the Environmental Research Laboratories in any advertising or sales promotion which would indicate or imply that the Environmental Research Laboratories approve, recommend, or endorse any proprietary product or proprietary material mentioned herein, or which has as its purpose an intent to cause directly or indirectly the advertised product to be used or purchased because of this Environmental Research Laboratories publication. Abstract A system of FORTRAN language computer programs is presented which have the ability to locate the sun at arbitrary times. On demand, the programs will return the distance and direction to the sun, either as seen by an observer at an arbitrary location on the Earth, or in a stan- dard astronomic coordinate system. For one century before or after the year 1960, the program is expected to have an accuracy of 30 seconds 5 of arc (2 seconds of time) in angular position, and 7 10 A.U. in distance. A non-standard algorithm is used which minimizes the number of trigonometric evaluations involved in the computations. 1 The NOAA Solar Ephemeris Program Albion D. Taylor National Oceanic and Atmospheric Administration Air Resources Laboratories Silver Spring, MD January 1981 Contents 1 Introduction 3 2 Use of the Solar Ephemeris Subroutines 3 3 Astronomical Terminology and Coordinate Systems 5 4 Computation Methods for the NOAA Solar Ephemeris 11 5 References 16 A Program Listings 17 A.1 SOLEFM . -
Do You Really Know What Time It Is? the Sun Doesn’T Work Around Your Watch
Solar Thermal Notebook John Siegenthaler, P.E. Do you really know what time it is? The sun doesn’t work around your watch. moving along its path through the sky. In other words, two observers within the same time zone and at essentially the same latitude (such as Boston and Detroit) will see the sun at different positions in the sky at the same indi- cated clock time. However, the sun will be in the same position in the sky when the solar time at both locations is the same. Thus, whenever you are using a symmetrical imaging device such as a solar path diagram, Solar Pathfinder or formulas that calculate the sun’s position as a function of time, that time needs to be solar time. Solar time can be calculated based on knowing local clock time using Formula 1 in combination with Figure 3 on Page 18. Formula 1: ܔ܉܋ܗۺ ۻ ܁ۺ ሻ۳ ۺି ۺାሺ ܂ୀܚ܉ܔܗܛ܂ Photo credit: ©istockphoto.com/Eric Gevaert The sun is directly above a true north/south line at solar noon. Where: Tsolar = solar time at the location ne of the first things you learn Figure 1 on Page 17) can help determine TLS = local standard time about planning and installing the time of day and month when the LM = longitude of the standard meridian solar thermal systems is the location will be shaded. for the time zone (°) O ܁ܗܔ܉ܚ ܂ ൌ ૢǣ െ ǣ ૢܕܑܖܝܜ܍ܛ ൌૢǣ ૠ܉Ǥ ܕǤ importance of orientation. On a theo- The vertically oriented time arcs on Llocal = longitude at the location (°) retically perfect clear sky day, a collector the dial of the Solar Pathfinder, as well as E = “Equation of time” (read from Figure array that faces true south will produce the times on a sun path diagram (such as 3; minutes) the greatest heat output, all other factors shown in Figure 2 on Page 17) are based being equal. -
Instructions for Use Mode D'emploi EQUATION of TIME Calibre 2120/2808 Selfwinding
Instructions for use Mode d’emploi EQUATION OF TIM E Calibre 2120/2808 Selfwinding 12 13 1 5 11 14 d 2 7 e 9 6 f 10 8 4 3 B C A B C ENGLISH 1. Introduction p 49 5. Basic functions p 78 The Manufacture Audemars Piguet Setting the time Generality Time-zone adjustments Winding the watch 2. About time p 56 Adjusting the perpetual calendar indications Times-zones Corrections if the watch has stopped for less than 3 days The units of time English Corrections if the watch has stopped for more The calendars than 3 days The earth’s coordinates Procedure for corrections 1. Date, day, month and leap year 3. Watch description p 62 2. The moon phase Views of the movement 3. The day Movement technical data 4. Sunrise, sunset and the equation of time of contents Table Specificities 5. Setting the time Watch indications and functions 6. Accessories p 83 4. Watch indications p 66 Rotating presentation case The perpetual calendar Setting stylus The astronomical moon The time equation 7. Additional comments p 85 True noon and mean noon Indication of sunrise and sunset times 46 47 The Manufacture h Audemars Piguet Englis The Vallée de Joux : cradle of the watchmaker’s art n the heart of the Swiss Jura, around 50 kilometres I north of Geneva, nestles a landscape which has retained its natural charm to this day : the Vallée de Joux. Around the mid-18th century, the harsh Introduction 1. climate of this mountainous region and soil depletion drove the farming community settled there to seek other sources of income. -
Euler's Forgotten Equation of the Center
Advances in Historical Studies, 2021, 10, 44-52 https://www.scirp.org/journal/ahs ISSN Online: 2327-0446 ISSN Print: 2327-0438 Euler’s Forgotten Equation of the Center Sylvio R. Bistafa University of São Paulo, São Paulo, Brazil How to cite this paper: Bistafa, S. R. Abstract (2021). Euler’s Forgotten Equation of the Center. Advances in Historical Studies, 10, In a 1778 publication in Latin, titled Nova Methodvs Motvm Planetarvm De- 44-52. terminandi (New method to determine the motion of planets), Euler derives https://doi.org/10.4236/ahs.2021.101005 an equation of the center, which, apparently, has been forgotten. In the present work, the developments that led to Euler’s equation of the center are Received: January 9, 2021 Accepted: March 12, 2021 revisited, and applied to three planets of the Solar System. These are then Published: March 15, 2021 compared with results obtained from an equation of center that has been proposed, showing good agreement for planets with not so high eccentrici- Copyright © 2021 by author(s) and ties. Nonetheless, Euler’s derivation was not influential, and since then, the Scientific Research Publishing Inc. resulting equation of the center has been neglected by scholars and by specia- This work is licensed under the Creative Commons Attribution International lized publications alike. License (CC BY 4.0). http://creativecommons.org/licenses/by/4.0/ Keywords Open Access Euler’s Works on Astronomy, Equation of the Center, History of Orbital Calculations, Investigations on Planets’ Orbits, Astronomical Calculations, Keplerian Orbital Mechanics 1. Introduction Since antiquity, the problem of predicting the motions of the heavenly bodies has been simplified by reducing it to one of a single body in orbit about another. -
19740004369.Pdf
IA-4 TheOrbitalMechanics of Fli_htMechanics A--A Am-m ---_._ _--_-_ :5::_¸¸¸:_:::_!_:_:_i:::_!:i:_:._::::_:i_;::::,::::,:::_:.:::i::i¸:5: ::':?::!:i:!:!:!:!::':i:i:::::::;_:;::_,.'__;_:::::::........... .... ===================================================: )) T .... -...: ==================================================================================================================================== ...... :::7:_))_):)):::_:i!._...............iii_i)))))))i)i):_::_)i0j))::::!:):::))))):)).." •.........)i'::::_).............!:!:i_)i::i)iii)))))i!_. L-73-3009 Apollo 9 Landing Module as viewed from the Comm_md Module in orbit over the earth. ii ! ,\ \ i ii-il NASASP-325 TheOrbitalMechanics of Fli_htMechanics RobertScottDunnin_ LangleyResearchCenter PreparedbyNASALangleyResearchCenter Scientific and Technical ln/ormation Office 1973 NATIONAL AERONAUTICS AND SPACE ADMINISTRATION _ Washington, D.C. If If 1 lf_;;_:'_,-li'-,,_,. A-AA A-I v_? V For sale by the National Technical Information Service Springfield, Virginia 22151 Price - Domestic, $4.75; Foreign, $7.25 Library of Congress Catalog Card Number 73-600091 ,WTT i di-ll PREFACE Despite the existence of numerous authoritative books in the field of orbital mechanics, the author has felt the need for a book which places emphasis on the con- ditions encountered with actively controlled satellites and spaceships rather than on observation and analysis of the passive heavenly bodies treated in classical astron- omy. Present-day space research, includiflg the use of computers, has made much of the material in previous books outmoded; less emphasis is now placed on closed-form solutions and more on iterative techniques. It is also apparent that a greater empha- sis on the basic formulas has become necessary. The problem of relative motion between two vehicles, which was rarely encountered in classical astronomy, has become a routine operational matter today and deserves consideration appropriate to its present importance. -
368-187 10 Q
~~ ~~ ~ ~ ~~ ~~ I . & UJJ-7- National Administration Goddard Space Flight Center Contract No. NAS-5-12487 ST - CM - 10687 ON ?HE MOTION OF REMOTE ARTIFICIAL EARTH'S SATELLITES IN 'ME GRAVITATIONAL FIELDS OF THE ENITH AND OF "€EMOON by V. P. Dolgachev * (USSR) 368-187 10 3 (ACCESSION NUMBER) 4 q P (PXGES) 'COW c 20 (CATEGORY) GPO PRICE $ io MARCH 1968 CFSTI PRICE(S) $ i .33 ' c5: Hard copy (HC) - v., Microfiche (MF) / 4,s- ff 653 July 65 1 .* . ST-(34-10687 ON 'IHE MOTION OF REMOTE ARTIFICIAL EARTH'S SATELLITES IN THE G.MVITATI0NA.L FIELDS OF THE EARTH AND OF THE MOON Vestnik Moskovskogo Universiteta by V. P. Dolgachev Astronomiya, No. 1, pp. 94 - 100, Izdatel'stvo MGU, 1968. SUMMARY The expressions are presented of first order perturbations of AES' orbit elements due to Earth's oblateness, and of the second harmonic of Moon's at- traction, the Moon being consicered as a material point moving along a circular orbit. The formulas derived are also valid for pert.urbations due to the Sun. * ** The expressions were derived in a preceding work [l] for secular varia- tions of remote AES in the gravitational fields of the Earth and of the Moon, whereupon perturbations from the second harmonic of the terrestrial potential and from the second and third harmonics of Moon's attraction were taken into account; it was moreover considered that the Moon is a material point moving along an elliptical orbit. Remaining within the framework of the classical scheme proposed by Lagran- ge, we obtained perturbations in the Lagrange elements; it is then natural that the formulas obtained for the secular perturbations are valid for small eccentricities and inclinations. -
Chapter 18 Time
CHAPTER 18 TIME TIME IN NAVIGATION 1800. Solar Time Sun will be on the observer’s meridian again when the Earth has moved to point C in its orbit. Thus, during the course of The Earth’s rotation on its axis causes the Sun and a day the Sun appears to move eastward with respect to the other celestial bodies to appear to move across the sky from stars. east to west each day. If a person located on the Earth’s The apparent positions of the stars are commonly equator measured the time interval between two successive reckoned with reference to an imaginary point called the transits overhead of a very distant star, he would be vernal equinox, the intersection of the celestial equator and measuring the period of the Earth’s rotation. If he then the ecliptic. The period of the Earth’s rotation measured made a similar measurement of the Sun, the resulting time with respect to the vernal equinox is called a sidereal day. would be about 4 minutes longer. This is due to the Earth’s The period with respect to the Sun is called an apparent motion around the Sun, which continuously changes the solar day. apparent place of the Sun among the stars. Thus, during the course of a day the Sun appears to move a little to the east When measuring time by the Earth’s rotation, using the among the stars, so that the Earth must rotate on its axis actual position of the Sun, or the apparent Sun, results in through more than 360° in order to bring the Sun overhead apparent solar time.