Quantifying the Differences Between Gravity Reduction Techniques

Total Page:16

File Type:pdf, Size:1020Kb

Quantifying the Differences Between Gravity Reduction Techniques CSIRO PUBLISHING Exploration Geophysics, 2018, 49, 735–743 https://doi.org/10.1071/EG17094 Quantifying the differences between gravity reduction techniques Philip Heath Geological Survey of South Australia, 4/101 Grenfell Street, Adelaide, SA 5000, Australia. Email: [email protected] Abstract. Gravity data processing (reduction) generally utilises the best-available formulae. New and improved formulae have been introduced over time and the resulting newly processed gravity will not match the old. Additionally, mistakes made in the gravity reduction process, as well as the incompatibilities between various equations, will inevitably lead to errors in the final product. This can mean that overlapping gravity surveys are often incompatible, leading to incorrect geological interpretations. In this paper I demonstrate the magnitude of change that results when different information is introduced at various stages of the gravity reduction process. I have focussed on differences relating to calibration factors, time zones and time changes, height, geodetic datums, gravity datums and the equations involved therein. The differences range from below the level of detection (0.01 mGal) to over 16.0 mGal. The results not only highlight the need to be diligent and thorough in processing gravity data, but also how it is necessary to document the steps taken when processing data. Without proper documentation, gravity surveys cannot be reprocessed should an error be identified. Key words: error, geodesy, gravity, processing, reduction. Received 28 July 2017, accepted 5 October 2017, published online 6 November 2017 Introduction Telford et al., 1990); however, these don’t contain comparisons A common product of Australian state and territory geological between what happens when equations of different vintage are surveys is a regional Bouguer gravity map. These images are used. Talwani (1998) discusses the errors involved in Bouguer compilations of multiple gravity surveys and it is an ongoing reduction, especially relating to the gravity effect of a spherical problem that overlapping surveys rarely match. Most commonly cap and Bullard B correction, which I have not replicated here. there appears to be an offset between the surveys, leading to A series of examples have been undertaken to illustrate mismatched points and anomalies in the final image. Numerous quantitatively how much difference is introduced at various attempts have been undertaken to create a smooth image of the stages of the gravity reduction process. Each demonstration gravity in South Australia using merging tools and different takes an element of the process, inserts realistic, but incorrect, gridding algorithms (e.g. Heath et al., 2012), but to date values and presents the results in a series of tables. a perfect image hasn’t been created. There are multiple reasons that surveys might mismatch. Method and results Different resolutions from different gravity meters as well as different precision and accuracy in elevation measurement Applying the scale factor techniques are two common issues. Another issue is how The scale factor (often referred to as a Calibration Factor; Heath, the data are processed. The process of gravity reduction is 2016) is a multiplication factor that must be applied to all raw straightforward; however, at each step of the process decisions gravity readings. A typical Scintrex CG5 gravity meter measures need to be made regarding which formulae to use, which gravity relative gravity values in mGal; however, the dynamic range of and geodetic datum is required and so on. This paper attempts the meter doesn’t match reality. As an illustrative example, to quantify some of the differences involved in using different two points on the Earth’s surface with the values 980 000 and equations. 980 100 mGal, respectively, have a difference of 100 mGal. In Multiple software packages exist (e.g. Intrepid Geophysics comparison, a gravity meter might measure 4000 and 4100.1 & Geosoft) that have the ability to process raw gravity data. mGal with a difference of 100.1 mGal. Therefore, a scaling factor In order to have full control over the reduction process I have must be calculated before all survey work by recording values at constructed a simple spreadsheet to undertake reduction in the the end points of a calibration range with a significant change field or in the office with minimal effort and to avoid software (typically over 50 mGal) in the gravity values. The scale factor (c) licensing issues. (The spreadsheet has been tested by undertaking is the ratio of the actual difference in gravity (Dga) to the measured gravity reduction using similar software and comparing results. difference in gravity (Dgm): The approach has allowed me to analyse the differences Dg involved at different stages of the gravity reduction process ¼ a : ð Þ c D 1 should erroneous information be input. It is freely available gm to anyone who requests it.) Raw gravity readings must be divided by the scale factor c. Many geophysical textbooks contain information regarding One potential source of error is using the inverse of the calibration the gravity reduction process (e.g. Blakely, 1995; Parasnis, 1962; factor (effectively multiplying instead of dividing by c). Journal compilation Ó ASEG 2018 Open Access CC BY-NC-ND www.publish.csiro.au/journals/eg 736 Exploration Geophysics P. Heath For a typical scale factor of 0.9997281, a typical raw reading of 7. Scale factor using best values only, treated as a gravity loop 3785.98 mGal becomes 3787.01 mGal if applied correctly and (from second ABA loop); and 3784.95 mGal if the inverse is used, creating a difference of 2.06 8. Scale factor using best values only, treated as a gravity loop mGal. The dynamic range of a Scintrex CG5 is 1000 to 9000 (ABABA). mGal, meaning this error could range from anywhere between For each calculation technique (listed 1 to 8 above) I’ve calculated 0.5 to 5.0 mGal (for the scale factor referred to here). the scale factor and the minimum and maximum corrected value of a CG5 gravity meter, assuming a dynamic range of 1000 to Methods to calculate c 9000 mGal. I’ve then calculated the difference between the values For the simplest approach, c can be calculated from two calculated from each scenario with the final scenario (which is measurements on the calibration range. It can also be calculated arguably the most accurate). The differences range from 0.01 to from an ABABA-type loop between two points A and B. In both ~1.00 mGal. Table 2 shows these results. cases the processor must decide to assume either a linear drift in Scenario 3 produces the least difference compared to Scenario the measurements, or to undertake a more thorough calculation to 8. Scenario 4 is effectively the same as Scenario 3, as it uses the determine the scale factor. Furthermore, the processor may have same method, just at a different time. Most of the scenarios multiple readings to choose from. If a CG5 is being used, does the produce a maximum difference in the range of 0.1 to 0.2 processor choose the readings with the lowest standard deviation mGal, with the greatest difference (1.0 mGal) resulting from (s.d.) or should they average them all? A single measurement on Scenario 2, where only two values are used to calculate the a CG5 gravity meter is actually an average of a series of readings; scale factor. hence, s.d. is available for each measurement. The following To illustrate how different scale factors affect a gravity survey, demonstration shows the effects of computing different scale consider the Coompana gravity survey (Allpike, 2017). The factors from the same set of observations. dynamic range of the survey is –64.59 to 19.20 mGal, a total Table 1 shows the raw data collected from a gravity calibration of ~84 mGal. This survey used three CG5 gravity meters, one run between the Kensington Gardens Sportsfield and Norton measuring at ~2500 mGals, one at 4000 mGals and one at 5000 Summit Cemetery, South Australia. mGals. I’ll call these gravity meters 1, 2 and 3, respectively, and Eight scenarios are considered, each a different way to I designate each gravity meter with its own scale factor from the calculate the calibration factor. The scenarios are: scenarios above. I assign gravity meter 1 the scale factor from 1. Scale factor using two ‘best’ values only (from first A and B scenario 2, gravity meter 2 the scale factor from scenario 5, and readings); gravity meter 3 the scale factor from scenario 8. If gravity meter 1 2. Scale factor using two average values (from first A and B measures values from 2458 to 2542 mGal (84 mGal around – readings); 2500 mGal), the scaled values become 2456.954- 2540.921 3. Scale factor using average values, assuming linear drift (from mGal, a difference of 83.964 mGal. Performing the same fi first ABA loop); operation for gravity meters 2 and 3, we nd scaled values of 4. Scale factor using average values, assuming linear drift (from 83.972 and 83.973 mGal, respectively. The maximum difference second ABA loop); here is 0.009 mGal, just under the 0.01 mGal level of detection. 5. Scale factor using average values, assuming linear drift (ABABA); Scale factor gravity datum 6. Scale factor using best values only, treated as a gravity loop The scale factor will also be different depending on the gravity (from first ABA loop); datum used for the known values in the calculation. Assuming Table 1. Raw readings taken from a scale factor run between Kensington Gardens (A) and Norton Summit Cemetery (B) using the CG5 gravity meter, serial number 050 800 135. ABA B A Reading s.d. Time Reading s.d.
Recommended publications
  • B3 : Variation of Gravity with Latitude and Elevation
    Geophysics 210 September 2008 B3 Variation of gravity with latitude and elevation By measuring the subtle changes in the acceleration of gravity from one place to another, it is possible to learn about changes in subsurface density. However, other factors can cause gravity to vary with position on the Earth. These effects must be removed from measurements in order to use gravity data to study the interior of the Earth. B3.1 Variation of gravity with latitude It is observed that at the Equator, g E = 978,033 mgal while at the poles g P = 983,219 mgal This difference is 5186 mgal, which is a lot larger than changes in gravity because of subsurface density. Can this observation be explained by the fact that the Earth is a rotating ellipsoid? (A)The Earth is distorted by rotation The Earth is an oblate spheroid. R E = 6378 km R P = 6357 km. Qualitative answer Since a point on the Equator is further from the centre of the Earth than the poles, gravity will be weaker at the Equator and g E < g P Quantitative answer GM E 24 For a sphere g (r) = where the mass of the Earth, ME = 5.957 10 kg. r 2 At the North Pole, RP = 6357 km and g P = 983,219 mgal. If we move up 21 km to the equator, the decrease in gravity will be 6467 mgal Thus g E = g P - 6467 mgal, which is too much to explain the observed difference between the Equator and the Poles. 1 Geophysics 210 September 2008 (B) - Centrifugal forces vary with latitude The rotation of the Earth also causes gravity to vary with latitude.
    [Show full text]
  • Instruments and Gravity Processing Drift and Tides
    Gravity 5 Objectives Instruments Gravity Gravity 5 Corrections Instruments and gravity processing Drift and Tides Latitude Free Air Chuck Connor, Laura Connor Atmosphere Simple Bouguer Summary Potential Fields Geophysics: Week 5 Further Reading EOMA Gravity 5 Objectives for Week 5 Gravity 5 Objectives Instruments • Gravity Learn about gravity Corrections instruments Drift and Tides • Learn about Latitude processing of gravity Free Air data Atmosphere • Make the Simple Bouguer corrections to Summary calculate a simple Further Bouguer anomaly Reading EOMA Gravity 5 The pendulum The first gravity data collected in the US were Gravity 5 obtained by G. Putman working for the Coast and Geodetic survey, around 1890. These gravity data comprised a set of 26 measurements made along a roughly E-W transect across the entire continental Objectives US. The survey took about 6 months to complete and was designed primarily to investigate isostatic Instruments compensation across the continent. Gravity Putnam used a pendulum gravity meter, based on the Corrections relation between gravity and the period of a pendulum: Drift and Tides 4π2l g = Latitude T 2 Free Air where: l is the length of the pendulum Atmosphere T is the pendulum period Simple Example Seems easy enough to obtain an absolute gravity Bouguer reading, but in practice pendulum gravity meters are Assuming the period of a pendulum is known to be 1 s Summary problematic. The length of the pendulum can change exactly, how well must the length of the pendulum be with temperature, the pendulum stand tends to sway, known to measure gravity to 10 mGal precision? Further air density effects the measurements, etc.
    [Show full text]
  • Preparation of Papers for AIAA Technical Conferences
    Gravity Modeling for Variable Fidelity Environments Michael M. Madden* NASA, Hampton, VA, 23681 Aerospace simulations can model worlds, such as the Earth, with differing levels of fidel- ity. The simulation may represent the world as a plane, a sphere, an ellipsoid, or a high- order closed surface. The world may or may not rotate. The user may select lower fidelity models based on computational limits, a need for simplified analysis, or comparison to other data. However, the user will also wish to retain a close semblance of behavior to the real world. The effects of gravity on objects are an important component of modeling real-world behavior. Engineers generally equate the term gravity with the observed free-fall accelera- tion. However, free-fall acceleration is not equal to all observers. To observers on the sur- face of a rotating world, free-fall acceleration is the sum of gravitational attraction and the centrifugal acceleration due to the world’s rotation. On the other hand, free-fall accelera- tion equals gravitational attraction to an observer in inertial space. Surface-observed simu- lations (e.g. aircraft), which use non-rotating world models, may choose to model observed free fall acceleration as the “gravity” term; such a model actually combines gravitational at- traction with centrifugal acceleration due to the Earth’s rotation. However, this modeling choice invites confusion as one evolves the simulation to higher fidelity world models or adds inertial observers. Care must be taken to model gravity in concert with the world model to avoid denigrating the fidelity of modeling observed free fall.
    [Show full text]
  • Gravity Anomalies - D
    GEOPHYSICS AND GEOCHEMISTRY – Vol.III - Gravity Anomalies - D. C. Mishra GRAVITY ANOMALIES D. C. Mishra National Geophysical Research Institute, Hyderabad, India Keywords: gravity anomalies, isostasy, Free Air and Bouguer gravity anomalies Contents 1. Introduction 2. Free Air and Bouguer Gravity Anomalies 3. Separation of Gravity Anomalies 3.1 Regional and Residual Gravity Fields 3.2 Separation Based on Surrounding Values 3.3 Polynomial Approximation 3.4 Digital Filtering 4. Analytical Operations 4.1 Continuation of the Gravity Field 4.2 Derivatives of the Gravity Field 5. Isostasy 5.1 Isostatic Regional and Residual Fields 5.2 Admittance Analysis and Effective Elastic Thickness 6. Interpretation and Modeling 6.1 Qualitative Interpretation and Some Approximate Estimates 6.2 Quantitative Modeling Due to Some Simple shapes 6.2.1 Sphere 6.2.2 Horizontal Cylinder 6.2.3 Vertical Cylinder 6.2.4 Prism 6.2.5 Contact 6.3 Gravity Anomaly Due to an Arbitrary Shaped Two-dimensional Body 6.4 Basement Relief Model 7. Applications 7.1 Bouguer Anomaly of Godavari Basin, India 7.2 Spectrum and Basement Relief 7.3 Modeling of Bouguer Anomaly of Godavari Basin Along a Profile 7.4 SomeUNESCO Special Applications – EOLSS Glossary Bibliography SAMPLE CHAPTERS Biographical Sketch Summary Gravity anomalies are defined in the form of free air and Bouguer anomalies. Various methods to separate them in the regional and the residual fields are described, and their limitations are discussed. Polynomial approximation and digital filtering for this purpose suffer from the arbitrary selection of the order of polynomial and cut off frequency, respectively. However, some constraints on the order of these anomalies can ©Encyclopedia of Life Support Systems (EOLSS) GEOPHYSICS AND GEOCHEMISTRY – Vol.III - Gravity Anomalies - D.
    [Show full text]
  • Tutorial Ellipsoid, Geoid, Gravity, Geodesy, and Geophysics
    GEOPHYSICS, VOL. 66, NO. 6 (NOVEMBER-DECEMBER 2001); P. 1660–1668, 4 FIGS., 3 TABLES. Tutorial Ellipsoid, geoid, gravity, geodesy, and geophysics Xiong Li∗ and Hans-Ju¨rgen Go¨tze‡ ABSTRACT surement we could make accurately (i.e., by leveling). Geophysics uses gravity to learn about the den- The GPS delivers a measurement of height above the sity variations of the Earth’s interior, whereas classical ellipsoid. In principle, in the geophysical use of gravity, geodesy uses gravity to define the geoid. This difference the ellipsoid height rather than the elevation should be in purpose has led to some confusion among geophysi- used throughout because a combination of the latitude cists, and this tutorial attempts to clarify two points of correction estimated by the International Gravity For- the confusion. First, it is well known now that gravity mula and the height correction is designed to remove anomalies after the “free-air” correction are still located the gravity effects due to an ellipsoid of revolution. In at their original positions. However, the “free-air” re- practice, for minerals and petroleum exploration, use of duction was thought historically to relocate gravity from the elevation rather than the ellipsoid height hardly in- its observation position to the geoid (mean sea level). troduces significant errors across the region of investi- Such an understanding is a geodetic fiction, invalid and gation because the geoid is very smooth. Furthermore, unacceptable in geophysics. Second, in gravity correc- the gravity effects due to an ellipsoid actually can be tions and gravity anomalies, the elevation has been used calculated by a closed-form expression.
    [Show full text]
  • Tutorial Ellipsoid, Geoid, Gravity, Geodesy, and Geophysics
    GEOPHYSICS, VOL. 66, NO. 6 (NOVEMBER-DECEMBER 2001); P. 1660Ð1668, 4 FIGS., 3 TABLES. Tutorial Ellipsoid,geoid,gravity,geodesy,andgeophysics XiongLi¤andHans-Ju¨ rgenGo¨ tzez ABSTRACT surement we could make accurately (i.e., by leveling). Geophysics uses gravity to learn about the den- The GPS delivers a measurement of height above the sity variations of the Earth’s interior, whereas classical ellipsoid. In principle, in the geophysical use of gravity, geodesy uses gravity to define the geoid. This difference the ellipsoid height rather than the elevation should be in purpose has led to some confusion among geophysi- used throughout because a combination of the latitude cists, and this tutorial attempts to clarify two points of correction estimated by the International Gravity For- the confusion. First, it is well known now that gravity mula and the height correction is designed to remove anomalies after the “free-air” correction are still located the gravity effects due to an ellipsoid of revolution. In at their original positions. However, the “free-air” re- practice, for minerals and petroleum exploration, use of duction was thought historically to relocate gravity from the elevation rather than the ellipsoid height hardly in- its observation position to the geoid (mean sea level). troduces significant errors across the region of investi- Such an understanding is a geodetic fiction, invalid and gation because the geoid is very smooth. Furthermore, unacceptable in geophysics. Second, in gravity correc- the gravity effects due to an ellipsoid actually can be tions and gravity anomalies, the elevation has been used calculated by a closed-form expression.
    [Show full text]
  • Imece2008-66518
    Proceedings of IMECE2008 2008 ASME International Mechanical Engineering Congress and Exposition October 31-November 6, 2008, Boston, Massachusetts, USA IMECE2008-66518 APPLICATION OF THE RAPID UPDATE CYCLE (RUC) TO AIRCRAFT FLIGHT SIMULATION Yan Zhang Seamus McGovern EG&G Technical Services U.S. DOT National Transportation Systems Center Cambridge, Massachusetts, USA Cambridge, Massachusetts, USA ABSTRACT ters for Environmental Prediction (NCEP), the National Oceanic An aircraft flight simulation model under development aims and Atmospheric Administration (NOAA), and produces numer- to provide a computer simulation tool to investigate aircraft flight ical weather prediction data hourly with horizontal spatial reso- performance during en route flight and landing under various lution of 20 km or 13 km, and vertical pressure resolution of 25 atmospherical conditions [1]. Within this model, the air pres- mb [4]. The RUC provides a broad range of environmental pa- sure and temperature serve as important parameters for deriv- rameters including, as a function of 37 constant pressure levels, ing the true airspeed (TAS). Also important are the wind speed the geopotential height, temperature, relative humidity, horizon- and direction, which will be direct inputs for the flight simulation tal wind velocity, and pressure vertical velocity. However, the model. air pressure is not provided in RUC data in terms of the geodetic In this paper, the Rapid Update Cycle (RUC) data, pro- location, rather it is used as the reference to specify other param- vided hourly by the National Centers for Environmental Predic- eters such as the geopotential height, temperature, wind veloc- tion (NCEP) and the National Oceanic and Atmospheric Admin- ity, etc., preventing the RUC data to be directly used for a given istration (NOAA) are used to derive the atmospherical param- geodetic location of an aircraft.
    [Show full text]
  • Evaluation of Accuracy of the Geodetic Reference Systems for the Modelling of Normal Gravity Fields of Nigeria
    www.ccsenet.org/apr Applied Physics Research Vol. 2, No. 2; November 2010 Evaluation of Accuracy of the Geodetic Reference Systems for the Modelling of Normal Gravity Fields of Nigeria A. A. Okiwelu (Corresponding author) Geophysics unit, Department of physics University of Calabar, Nigeria Tel: 234-803-400-3637 E-mail: [email protected] E. E. Okwueze Geophysics Unit, Department of Physics University of Calabar, Nigeria Tel: 234-803-543-2338 E-mail: [email protected] C. E. Onwukwe Department of Maths/Statistics and Computer Science University of Calabar, Nigeria Tel: 234-803-713-4718 E-mail: [email protected] Abstract The normal gravity fields of Nigeria have been modeled exploiting the Geodetic Reference System 1930 (GRS-30), Geodetic reference system 1967 (GRS-1967) and the world geodetic reference system 1984 (WGS-84). The determination of the normal gravity fields from the three Geodetic Reference Systems were carried out to evaluate the accuracy of one reference datum with respect to another. Descriptive statistics of the normal gravity field values modeled on regional and local scales showed a large difference (16.11mGal ) between the 1930 reference earth model (GRS-30) and 1967 reference earth model (GRS-67). A large difference was also established between the 1930 and 1984 reference earth models. The large difference in the mean of normal gravity field is attributed to error inherent in the Potsdam value (16mGal ). However, the small difference in normal gravity field values between the 1967 and 1984 reference systems is a pointer that the choice of either application in geophysical exploration or geodetic applications is of minor importance.
    [Show full text]
  • DOİ:10.5578/Fmbd.67502 the Comparison of Gravity Anomalies
    Afyon Kocatepe Üniversitesi Fen ve Mühendislik Bilimleri Dergisi Afyon Kocatepe University Journal of Science and Engineering AKÜ FEMÜBİD 18 (2018) 015504 (981-990) AKU J. Sci. Eng. 18 (2018) 015504 (981-990) DOİ: 10.5578/fmbd.67502 Araştırma Makalesi / Research Article The Comparison of Gravity Anomalies based on Recent High-Degree Global Models Mustafa Yılmaz1,*, Bürhan Kozlu2 1 Afyon Kocatepe Üniversitesi, Mühendislik Fakültesi, Harita Mühendisliği Bölümü, Merkez-Afyonkarahisar, Türkiye 2 Şenoğlu Harita Ticaret Limited Şirketi, Soma-Manisa, Türkiye *Corresponding author, e-mail: [email protected] Geliş Tarihi:03.07.2018 ; Kabul Tarihi:03.12.2018 Abstract The Earth system generates different phenomena that are observable at the surface of the Earth such as: Mass deformations and displacements leading to plate tectonics, earthquakes, and volcanism. The dynamic processes associated with the interior, surface, and atmosphere of the Earth affect the three pillars of geodesy: Shape of the Earth, its gravity field, and its rotation. Geodesy establishes a characteristic structure in order to define, monitor, and predict of the whole Earth system. The traditional and new instruments, observable, and techniques in geodesy are related to the gravity field. Keywords Therefore, the geodesy monitors the gravity field and its temporal variability in order to transform the Free-air gravity anomaly; geodetic observations made on the physical surface of the Earth into the geometrical surface in which Bouguer gravity anomaly; positions are mathematically defined. In this paper, the main components of the gravity field modelling, Global model; (Free-air and Bouguer) gravity anomalies are calculated via recent high-degree global models Land gravity.
    [Show full text]
  • By Urho Antti Kalevl Uotila I960
    Copyright "by Urho Antti Kalevl Uotila i960 INVESTIGATIONS ON THE GRAVITY FIELD AND SHAPE OF THE EARTH DISSERTATION Presented in Partial Fulfillment of the Requirements for the Degree Doctor of Philosophy In the Graduate School of The Ohio State University By URHO ANTTI KALEVI UOTILA, M.Sc. ****** The Ohio State University 1959 Approved hy: W , R Adviser Department of Geology (Geodetic Sciences) ii PREFACE Geodetic science, as Dr. Welkko A. Heiskanen has long maintained, has had a great need for a world-wide geodetic system which would connect the different regional geodetic systems of the world. In recent years, the need of such a globe-spanning system has also been increasingly recognized by the Armed Services, particularly the United States Air Force, as a basis for obtaining the accurate distances and directions so important to our national defense In this Jet flight era. These needs, the academic and the military, were admirably combined with the establishment In 1950 of the World-Wide Gravity Project by Dr. Heiskanen, under the sponsorship of the United States Air Force, at the Mapping and Charting Research Laboratory of The Ohio State University Research Foundation. Under this significant program, observational gravity data from various agencies all over the world were, and continue to be, channeled into Columbus, adjusted to one reference system (the Potsdam system), translated Into mean free air gravity anomalies, and finally used for computations of the undulations of the geold and the deflection of the vertical. Because of the vast amounts of observational data handled by the Laboratory and the complexity of the computations Involved, the writer Ill had the opportunity to develop a variety of new methods and techniques particularly as pertains to high-speed computational operations.
    [Show full text]
  • Comparison of Theoretical and Measured Acceleration Due to Gravity
    ISSN(Online) : 2319-8753 ISSN (Print) : 2347-6710 International Journal of Innovative Research in Science, Engineering and Technology (An ISO 3297: 2007 Certified Organization) Vol. 5, Issue 3, March 2016 Comparison of Theoretical and Measured Acceleration Due to Gravity Mujahid Hassan Sani1, Jamilu Tijjani Baraya2, Sunusi Mohammed Mu’awuya3, Auwal Abdulkarim4 P.G. Student, Department of Physics, Jodhpur National University, Jodhpur, Rajasthan, India1 P.G. Student, Department of Physics, Jodhpur National University, Jodhpur, Rajasthan, India2 P.G. Student, Department of Physics, Jodhpur National University, Jodhpur, Rajasthan, India3 P.G. Student, Department of Physics, Jodhpur National University, Jodhpur, Rajasthan, India4 ABSTRACT: The earth gravity pulls everything on or near the planet towards its centre. The force responsible for this pull is called the gravitational force and it varies from place to place. This paper work presents the experimental value of theoretical acceleration due to gravity g which was obtained in five (5) different locations and their average was also obtained as 9.655678 m/s2, also the value of theoretical acceleration due to gravity g was obtained in that five (5) different locations where their average was obtained as 9.7897034 m/s2. By comparing the two it was found that the theoretical value leads the experimental value by 0.1340254 m/s2 which were due to experimental errors. KEYWORDS: Acceleration, pendulum bob, latitude, Altitude. I. INTRODUCTION The acceleration due to gravity is the most fundamental parameter in Physics. The motion of object on the earth’s surface, atmosphere, etc. is governed by the earth’s gravity. Earth’s gravity is the force with which the earth attracts the object towards its centre.
    [Show full text]
  • On Different Techniques for the Calculation of Bouguer Gravity
    University of Texas at El Paso DigitalCommons@UTEP Open Access Theses & Dissertations 2013-01-01 On Different Techniques For The alcC ulation Of Bouguer Gravity Anomalies For Joint Inversion And Model Fusion Of Geophysical Data In The Rio Grande Rift Azucena Zamora University of Texas at El Paso, [email protected] Follow this and additional works at: https://digitalcommons.utep.edu/open_etd Part of the Applied Mathematics Commons, and the Geophysics and Seismology Commons Recommended Citation Zamora, Azucena, "On Different Techniques For The alcC ulation Of Bouguer Gravity Anomalies For Joint Inversion And Model Fusion Of Geophysical Data In The Rio Grande Rift" (2013). Open Access Theses & Dissertations. 1965. https://digitalcommons.utep.edu/open_etd/1965 This is brought to you for free and open access by DigitalCommons@UTEP. It has been accepted for inclusion in Open Access Theses & Dissertations by an authorized administrator of DigitalCommons@UTEP. For more information, please contact [email protected]. ON DIFFERENT TECHNIQUES FOR THE CALCULATION OF BOUGUER GRAVITY ANOMALIES FOR JOINT INVERSION AND MODEL FUSION OF GEOPHYSICAL DATA IN THE RIO GRANDE RIFT AZUCENA ZAMORA Program in Computational Science APPROVED: Aaron Velasco, Chair, Ph.D. Rodrigo Romero, Ph.D. Vladik Kreinovich, Ph.D. Benjamin C. Flores, Ph.D. Dean of the Graduate School Para mi familia con amor Sin ustedes nada de esto seria posible ON DIFFERENT TECHNIQUES FOR THE CALCULATION OF BOUGUER GRAVITY ANOMALIES FOR JOINT INVERSION AND MODEL FUSION OF GEOPHYSICAL DATA
    [Show full text]