Lunar Deflections of the Vertical and Their Distribution
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Exploration of the Moon
Exploration of the Moon The physical exploration of the Moon began when Luna 2, a space probe launched by the Soviet Union, made an impact on the surface of the Moon on September 14, 1959. Prior to that the only available means of exploration had been observation from Earth. The invention of the optical telescope brought about the first leap in the quality of lunar observations. Galileo Galilei is generally credited as the first person to use a telescope for astronomical purposes; having made his own telescope in 1609, the mountains and craters on the lunar surface were among his first observations using it. NASA's Apollo program was the first, and to date only, mission to successfully land humans on the Moon, which it did six times. The first landing took place in 1969, when astronauts placed scientific instruments and returnedlunar samples to Earth. Apollo 12 Lunar Module Intrepid prepares to descend towards the surface of the Moon. NASA photo. Contents Early history Space race Recent exploration Plans Past and future lunar missions See also References External links Early history The ancient Greek philosopher Anaxagoras (d. 428 BC) reasoned that the Sun and Moon were both giant spherical rocks, and that the latter reflected the light of the former. His non-religious view of the heavens was one cause for his imprisonment and eventual exile.[1] In his little book On the Face in the Moon's Orb, Plutarch suggested that the Moon had deep recesses in which the light of the Sun did not reach and that the spots are nothing but the shadows of rivers or deep chasms. -
Fitting Gravimetric Geoid Models to Vertical Deflections
Journal of Geodesy (submitted) 1 Fitting gravimetric geoid models to vertical deflections 2 3 W.E. Featherstone ( ) 4 Western Australian Centre for Geodesy & The Institute for Geoscience Research, 5 Curtin University of Technology, GPO Box U1987, Perth, WA 6845, Australia 6 Tel: +61 8 9266-2734; Fax: +61 8 9266-2703; Email: [email protected] 7 8 D.D. Lichti 9 Department of Geomatics Engineering & The Centre for Bioengineering Research and 10 Education, Schulich School of Engineering, The University of Calgary, 11 2500 University Drive NW, Calgary, Alberta, T2N 1N4, Canada 12 Tel: +1 403 210-9495; Fax: +1 403 284 1980; Email: [email protected] 13 14 Abstract . Regional gravimetric geoid and quasigeoid models are now commonly fitted 15 to GPS-levelling data, which simultaneously absorbs levelling, GPS and quasi/geoid 16 errors due to their inseparability. We propose that independent vertical deflections are 17 used instead, which are not affected by this inseparability problem. The formulation is 18 set out for geoid slopes and changes in slopes. Application to 1080 astrogeodetic 19 deflections over Australia for the AUSGeoid98 model shows that it is feasible, but the 20 poor quality of the historical astrogeodetic deflections led to some unrealistic values. 21 22 Keywords : Gravimetric geoid errors, vertical deflections, vertical datum errors 23 24 1. Introduction 25 Fitting regional gravimetric geoid or quasigeoid models to GPS-levelling data has 26 become a widespread practice. A principal objection to this is the inseparability of 27 errors among the levelling and local vertical datum (LVD), GPS and gravimetric 28 quasi/geoid model (cf. -
The Deflection of the Vertical, from Bouguer to Vening-Meinesz, and Beyond – the Unsung Hero of Geodesy and Geophysics
EGU21-596 https://doi.org/10.5194/egusphere-egu21-596 EGU General Assembly 2021 © Author(s) 2021. This work is distributed under the Creative Commons Attribution 4.0 License. The Deflection of the Vertical, from Bouguer to Vening-Meinesz, and Beyond – the unsung hero of geodesy and geophysics Christopher Jekeli Ohio State University, School of Earth Sciences, Division of Geodetic Science, United States of America ([email protected]) When thinking of gravity in geodesy and geophysics, one usually thinks of its magnitude, often referred to a reference field, the normal gravity. It is, after all, the free-air gravity anomaly that plays the significant role in terrestrial data bases that lead to Earth Gravitational Models (such as EGM96 or EGM2008) for a multitude of geodetic and geophysical applications. It is the Bouguer anomaly that geologists and exploration geophysicists use to infer deep crustal density anomalies. Yet, it was also Pierre Bouguer (1698-1758) who, using the measured direction of gravity, was the first to endeavor a determination of Earth’s mean density (to “weigh the Earth”), that is, by observing the deflection of the vertical due to Mount Chimborazo in Ecuador. Bouguer’s results, moreover, sowed initial seeds for the theories of isostasy. With these auspicious beginnings, the deflection of the vertical has been an important, if not illustrious, player in geodetic history that continues to the present day. Neglecting the vertical deflection in fundamental surveying campaigns in the mid to late 18th century (e.g., Lacaille in South Africa and Méchain and Delambre in France) led to errors in the perceived shape of the Earth, as well as its scale that influenced the definition of the length of a meter. -
Lunar Satellite Attitude Determination System
Lunar Satellite Attitude Determination System SENIOR DESIGN PROPOSAL PRESENTATION TEAM EPOCH KUPOLUYI, TOLULOPE (LEAD DEVELOPER) SONOIKI, OLUWAYEMISI (LEAD RESEARCHER) WARREN, DANAH (PROJECT MANAGER) NOVEMBER 13, 2009 Outline 1. Background 2. Problem Formulation 3. Current Status of Art 4. Solution Approaches 5. Tasks 6. Project Management 7. Verification Plan & Deliverables 8. Costs and Resources 9. Conclusion 10. Questions Background: Lunar Satellites Manned (Orbital and suborbital) & Unmanned (Earth Orbit and Lunar Orbit) Lunar Satellites include: y Clementine—US Navy mission, orbited Moon, detected hydrogen at the poles y Luna 1—first lunar flyby y Luna 2—first lunar impact y Luna 3—first images of lunar far side y Luna 9—first soft landing on the Moon y Luna 10—first lunar orbiter y Luna 16—first unmanned lunar sample retrieval y Lunar Orbiter—very successful series of lunar mapping spacecraft y Lunar Prospector—confirmed detection of hydrogen at the lunar poles y SMART-1 ESA—Lunar Impact y Surveyor—first USA soft lander y Chandrayaan 1 —first Indian Lunar mission Background: Attitude Determination y Spacecraft: A vehicle intended to be launched into space. y Attitude: Orientation in space or transformation between a body frame and a reference frame. y Attitude determination: Computing the spacecraft attitude from optical sensor measurements and ephemeris information. (Sun, Stars, Earth, Moon) WHY ? Torques (Disturbance) y Gravity gradient y Solar radiation y Atmospheric drag y Magnetic torque y Internal Forces Background: Systems Closed loop (actuators controlled on board), Active (uses electricity or propellant). Problem Formulation y Customer wants to fly a simple, low- cost spacecraft near the Moon. -
The Moon As a Laboratory for Biological Contamination Research
The Moon As a Laboratory for Biological Contamina8on Research Jason P. Dworkin1, Daniel P. Glavin1, Mark Lupisella1, David R. Williams1, Gerhard Kminek2, and John D. Rummel3 1NASA Goddard Space Flight Center, Greenbelt, MD 20771, USA 2European Space AgenCy, Noordwijk, The Netherlands 3SETI InsQtute, Mountain View, CA 94043, USA Introduction Catalog of Lunar Artifacts Some Apollo Sites Spacecraft Landing Type Landing Date Latitude, Longitude Ref. The Moon provides a high fidelity test-bed to prepare for the Luna 2 Impact 14 September 1959 29.1 N, 0 E a Ranger 4 Impact 26 April 1962 15.5 S, 130.7 W b The microbial analysis of exploration of Mars, Europa, Enceladus, etc. Ranger 6 Impact 2 February 1964 9.39 N, 21.48 E c the Surveyor 3 camera Ranger 7 Impact 31 July 1964 10.63 S, 20.68 W c returned by Apollo 12 is Much of our knowledge of planetary protection and contamination Ranger 8 Impact 20 February 1965 2.64 N, 24.79 E c flawed. We can do better. Ranger 9 Impact 24 March 1965 12.83 S, 2.39 W c science are based on models, brief and small experiments, or Luna 5 Impact 12 May 1965 31 S, 8 W b measurements in low Earth orbit. Luna 7 Impact 7 October 1965 9 N, 49 W b Luna 8 Impact 6 December 1965 9.1 N, 63.3 W b Experiments on the Moon could be piggybacked on human Luna 9 Soft Landing 3 February 1966 7.13 N, 64.37 W b Surveyor 1 Soft Landing 2 June 1966 2.47 S, 43.34 W c exploration or use the debris from past missions to test and Luna 10 Impact Unknown (1966) Unknown d expand our current understanding to reduce the cost and/or risk Luna 11 Impact Unknown (1966) Unknown d Surveyor 2 Impact 23 September 1966 5.5 N, 12.0 W b of future missions to restricted destinations in the solar system. -
Small Satellite Earth-To-Moon Direct Transfer Trajectories Using the CR3BP
Scholars' Mine Masters Theses Student Theses and Dissertations Fall 2019 Small satellite earth-to-moon direct transfer trajectories using the CR3BP Garrett Levi McMillan Follow this and additional works at: https://scholarsmine.mst.edu/masters_theses Part of the Aerospace Engineering Commons Department: Recommended Citation McMillan, Garrett Levi, "Small satellite earth-to-moon direct transfer trajectories using the CR3BP" (2019). Masters Theses. 7920. https://scholarsmine.mst.edu/masters_theses/7920 This thesis is brought to you by Scholars' Mine, a service of the Missouri S&T Library and Learning Resources. This work is protected by U. S. Copyright Law. Unauthorized use including reproduction for redistribution requires the permission of the copyright holder. For more information, please contact [email protected]. SMALL SATELLITE EARTH-TO-MOON DIRECT TRANSFER TRAJECTORIES USING THE CR3BP by GARRETT LEVI MCMILLAN A THESIS Presented to the Graduate Faculty of the MISSOURI UNIVERSITY OF SCIENCE AND TECHNOLOGY In Partial Fulfillment of the Requirements for the Degree MASTER OF SCIENCE in AEROSPACE ENGINEERING 2019 Approved by: Dr. Henry Pernicka, Advisor Dr. David Riggins Dr. Serhat Hosder Copyright 2019 GARRETT LEVI MCMILLAN All Rights Reserved iii ABSTRACT The CubeSat/small satellite field is one of the fastest growing means of space exploration, with applications continuing to expand for component development, commu- nication, and scientific research. This thesis study focuses on establishing suitable small satellite Earth-to-Moon direct-transfer trajectories, providing a baseline understanding of their propulsive demands, determining currently available off-the-shelf propulsive technol- ogy capable of meeting these demands, as well as demonstrating the effectiveness of the Circular Restricted Three Body Problem (CR3BP) for preliminary mission design. -
Scientific Exploration of the Moon
Scientific Exploration of the Moon DR FAROUK EL-BAZ Research Director, Center for Earth and Planetary Studies, Smithsonian Institution, Washington, DC, USA The exploration of the Moon has involved a highly successful interdisciplinary approach to solving a number of scientific problems. It has required the interactions of astronomers to classify surface features; cartographers to map interesting areas; geologists to unravel the history of the lunar crust; geochemists to decipher its chemical makeup; geophysicists to establish its structure; physicists to study the environment; and mathematicians to work with engineers on optimizing the delivery to and from the Moon of exploration tools. Although, to date, the harvest of lunar science has not answered all the questions posed, it has already given us a much better understanding of the Moon and its history. Additionally, the lessons learned from this endeavor have been applied successfully to planetary missions. The scientific exploration of the Moon has not ended; it continues to this day and plans are being formulated for future lunar missions. The exploration of the Moon undoubtedly started Moon, and Luna 3 provided the first glimpse of the with the naked eye at the dawn of history,1 when lunar far side. After these significant steps, the mankind hunted in the wilderness and settled the American space program began its contribution to earliest farms. Our knowledge of the Moon took a lunar exploration with the Ranger hard landers' quantum jump when Galileo Galilei trained his from 1964 to 1965. These missions provided us with telescope toward it. Since then, generations of the first close-up views (nearly 0.3 m resolution) of researchers have followed suit utilizing successively the lunar surface by transmitting pictures until just more complex instruments." The most significant before crashing.6 The pictures confirmed that the quantum jump in the knowledge of our only natural lunar dark areas, the maria, were relatively flat and satellite came with the advent of the space age, topographically simple. -
Toolbox for Analysis of Flexural Isostasy (TAFI)—A MATLAB Toolbox for Modeling Flexural Deformation of the Lithosphere GEOSPHERE; V
Software Contribution GEOSPHERE Toolbox for Analysis of Flexural Isostasy (TAFI)—A MATLAB toolbox for modeling flexural deformation of the lithosphere GEOSPHERE; v. 13, no. 5 Sumant Jha, Dennis L. Harry, and Derek L. Schutt Department of Geosciences, Colorado State University, 1482 Campus Delivery, Fort Collins, Colorado 80523, USA doi:10.1130/GES01421.1 7 figures; 5 tables; 2 supplemental files ABSTRACT typically involving subsidence in the vicinity of the load (assuming the load represents an addition of weight to the lithosphere) and uplift in surrounding CORRESPONDENCE: sumant .jha@colostate .edu This paper describes a new interactive toolbox for the MATLAB computing areas (the peripheral “bulge”) (Fig. 1). The magnitude and wavelength of the platform called Toolbox for Analysis of Flexural Isostasy (TAFI). TAFI supports flexural deflection depends on the magnitude of the load and the strength of CITATION: Jha, S., Harry, D.L., and Schutt, D.L., two- and three-dimensional (2-D and 3-D) modeling of flexural subsidence the lithosphere, with greater strength resulting in more broadly distributed 2017, Toolbox for Analysis of Flexural Isostasy (TAFI)—A MATLAB toolbox for modeling flexural and uplift of the lithosphere in response to vertical tectonic loading. Flexural (larger-wavelength) deformation. Flexure results in variations in the regional defor ma tion of the lithosphere: Geosphere, v. 13, deformation is approximated as bending of a thin elastic plate overlying an gravity field due to deformation of density interfaces within the lithosphere. no. 5, p. 1555–1565, doi:10.1130/GES01421.1. inviscid fluid asthenosphere. The associated gravity anomaly is calculated by Such density interfaces may include the crust-mantle boundary, the interface summing the anomalies produced by flexure of each density interface within between the sedimentary basin fill and underlying rocks, the seafloor in marine Received 26 August 2016 the lithosphere, using Parker’s algorithm. -
An Analysis of Vertical Deflections Derived from High-Degree Spherical
Journal of Geodesy (1999) 73: 10 ± 22 An analysis of vertical de¯ections derived from high-degree spherical harmonic models C. Jekeli Department of Civil and Environmental Engineering and Geodetic Science, The Ohio State University, 2070 Neil Ave, Columbus, OH 43210, USA e-mail: [email protected]; Tel.: +1 614 292 7117; Fax: +1 614 292 2957 Received: 9 December 1997 / Accepted: 21 August 1998 Abstract. The theoretical dierences between the Hel- from the obvious limited resolution imposed by the mert de¯ection of the vertical and that computed from a degree of truncation, vertical de¯ections from spherical truncated spherical harmonic series of the gravity ®eld, harmonic models dier, in principle, from their geomet- aside from the limited spectral content in the latter, ric counterpart mostly because of the curvature of the include the curvature of the normal plumb line, the normal plumb line. This is a systematic eect that is permanent tidal eect, and datum origin and orientation usually small, but may be signi®cant at very high ¯ight osets. A numerical comparison between de¯ections altitudes: for example, if the spherical harmonic models derived from spherical harmonic model EGM96 and are used to compensate inertial navigation systems astronomic de¯ections in the conterminous United (INS) for the eects of gravitation. A rigorous compar- States (CONUS) shows that correcting these systematic ison is presented here that identi®es this and all other eects reduces the mean dierences in some areas. dierences, including the question of permanent tide Overall, the mean dierence in CONUS is reduced from eects. -
North American Air Defense Command (NORAD), Weekly
r . D~ L.-A-5$ -1F)f0 N 1_'--f~Ju L fl1 1 DECLASSIFIED UN DER AUTHORITY OF THE INTERAGENCY SECURITY CLASSIFICATION APPEALS PANEL, E.O. 13526, SECTION 5.3(b)(3) ISCAP APPEAL NO. 2009-068, document no. 130 DECLASSIFICATION DATE: February 25, 2015 6 . ... ff : ' ~. ~~ ial (~~ ·' ~··. :· --- ).:. :.~ , . ,~ : ~ ~ s 1 ;,, .y.~ :FOR OfF ICtAl USE ONLY ...... ~ ~ WIR 23/66 -- .. 10 Jun 66 JUN 13 196 6 - . - . j Posta l Registry N o .~·:? ,{:f~ fc NO Issue No. Z3/66, 10 June 1966 . IR mBrief 3 I 5 3 16 4 22 4 Portion identified as non responsive to the appeal 23 5 ( 26 Portion identified as no n responsive to the appea l 27 5 7 27 8 28 8 ~--------------------------~ 9 FAILURE OF 27 :\U.RCH TENTATIVELY ASSESSED AS MO Li'iiYA ATTEMPT 1 0 P ropulsion telemetry basis fo r estimate. LUNA l 0 CEASES TRANSMITTING 2 MONTHS AFTER LAUNCH 10 Soviets make·final report. ELL\41NATION OF WIRING TO COSMONAUTS' BIOSENSORS SOUGHT 12 Would increase their mobility. COVER: Low- speed wind tunneL at Zhukovskiy RECENT INTERCEPTS OF SOVIET SPACE-VEHICLE Central Aerodynamic Institute. On the TRANSMISSIONS 12 stand is a quarter - scale model of the AN-22. (Fr om Nedelya) (OF.FICIAL USE ONLY) NOTE: Pages 32 , 34, 35, 38, .39 and 42 of this issue are blank. - ] - SECRET sign ificant intelligence on space developments and trends Failure of 27 March Tentatively Assessed as Mol niya Attempt A vehicle launched from Tyuratam on 2 7 March but which failed to achieve orbit is now tentatively assessed as an attempt to launch a Molniya-type 12-hour communications satellite. -
GRAIL): Mapping the Lunar Interior from Crust to Core
Space Sci Rev DOI 10.1007/s11214-012-9952-7 Gravity Recovery and Interior Laboratory (GRAIL): Mapping the Lunar Interior from Crust to Core Maria T. Zuber · David E. Smith · David H. Lehman · Tom L. Hoffman · Sami W. Asmar · Michael M. Watkins Received: 1 September 2012 / Accepted: 26 November 2012 © Springer Science+Business Media Dordrecht 2012 Abstract The Gravity Recovery and Interior Laboratory (GRAIL) is a spacecraft-to- spacecraft tracking mission that was developed to map the structure of the lunar interior by producing a detailed map of the gravity field. The resulting model of the interior will be used to address outstanding questions regarding the Moon’s thermal evolution, and will be applicable more generally to the evolution of all terrestrial planets. Each GRAIL orbiter contains a Lunar Gravity Ranging System instrument that conducts dual-one-way ranging measurements to measure precisely the relative motion between them, which in turn are used to develop the lunar gravity field map. Each orbiter also carries an Education/Public Outreach payload, Moon Knowledge Acquired by Middle-School Students (MoonKAM), in which middle school students target images of the Moon for subsequent classroom anal- ysis. Subsequent to a successful launch on September 10, 2011, the twin GRAIL orbiters embarked on independent trajectories on a 3.5-month-long cruise to the Moon via the EL-1 Lagrange point. The spacecraft were inserted into polar orbits on December 31, 2011 and January 1, 2012. After a succession of 19 maneuvers the two orbiters settled into precision formation to begin science operations in March 1, 2012 with an average altitude of 55 km. -
Catherine L. Mayes, David T. Sandwell, and Lawrence A. Lawver
PALEOCEANOGRAPHIC MAPPING PROJECT L i t;~- ...1 ''\1 ! ~f; ,.- F PROGRESS REPORT No. 43 - 0888 '··· ; (.c:- F-;.-:.... Tectonic History and New Isochron Chart of the South Pacific by Catherine L. Mayes, David T. Sandwell, and Lawrence A. Lawver University of Texas Institute for Geophysics Technical Report No. 95 TECfONIC HISTORY AND NEW ISOCHR.ON CHART OF THE SOUTH PACIFIC Catherine L. Mayes 1,2 David T. Sandwell2 and Lawrence A. Lawver 2 1 The Department of Geological Sciences and Instititue for Geophysics, P.O. Box 7456, University of Texas at Austin, Austin, Texas 78713-7456 2 Institute for Geophysics, University of Texas at Austin, 8701 Mopac Blvd., Austin, Texas 78751 Submitted to: Journal of Geophysical Research May, 1988 1 ABS1RACf We have developed an internally consistent isochron chart and a tectonic history of the South Pacific using a combination of new satellite altimeter data and shipboard magnetic and bathymetric data. Highly accurate, vertical deflection profiles (1-2 Jlrad), derived from 22 repeat cycles of Geosat altimetry, reveal subtle lineations in the gravity field associated with the South Pacific fracture zones. These fracture zone lineations are correlated with sparse shipboard bathymetric identifications of fracture zones and thus can be used to determine paleo-spreading directions in uncharted areas. The high density of Geosat altimeter profiles reveals previously unknown details in paleo-spreading directions on all of the major plates. Magnetic anomaly identifications and magnetic lineation interpretations from published sources were combined with these fracture zone lineations to produce a tectonic fabric map. Tne tectonic fabric was then used to derive new plate reconstructions for twelve selected times in the Late Cretaceous and Cenozoic.