# Theoretical gravity

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Mathematical model of Earth's gravity

In [geodesy](/source/Geodesy) and [geophysics](/source/Geophysics), **theoretical gravity** or **normal gravity** is an approximation of [Earth's gravity](/source/Earth's_gravity), on or near its surface, by means of a [mathematical model](/source/Mathematical_model). The most common theoretical model is a rotating [Earth ellipsoid](/source/Earth_ellipsoid) of revolution (i.e., a [spheroid](/source/Spheroid)).

Other representations of gravity can be used in the study and analysis of other bodies, such as [asteroids](/source/Asteroid). Widely used representations of a gravity field in the context of geodesy include [spherical harmonics](/source/Spherical_harmonics), mascon models, and polyhedral gravity representations.[1]

## Principles

This section may need to be cleaned up. It has been merged from Gravitational acceleration.

The type of gravity model used for the Earth depends upon the degree of fidelity required for a given problem. For many problems such as aircraft simulation, it may be sufficient to consider gravity to be a constant, defined as:[2]

- g = g 45 = {\displaystyle g=g_{45}=} 9.80665 m/s2 (32.1740 ft/s2)

based upon data from *World Geodetic System 1984* ([WGS-84](/source/World_Geodetic_System)), where g {\displaystyle g} is understood to be pointing 'down' in the local frame of reference.

If it is desirable to model an object's weight on Earth as a function of [latitude](/source/Latitude), one could use the following:[2]: 41

- g = g 45 − 1 2 ( g p o l e s − g e q u a t o r ) cos ⁡ ( 2 φ ⋅ π 180 ) {\displaystyle g=g_{45}-{\tfrac {1}{2}}(g_{\mathrm {poles} }-g_{\mathrm {equator} })\cos \left(2\,\varphi \cdot {\frac {\pi }{180}}\right)}

where

- g p o l e s {\displaystyle g_{\mathrm {poles} }} = 9.832 m/s2 (32.26 ft/s2)

- g 45 {\displaystyle g_{45}} = 9.806 m/s2 (32.17 ft/s2)

- g e q u a t o r {\displaystyle g_{\mathrm {equator} }} = 9.780 m/s2 (32.09 ft/s2)

- φ {\displaystyle \varphi } = latitude, between −90° and +90°

Neither of these accounts for changes in gravity with changes in altitude, but the model with the cosine function does take into account the centrifugal relief that is produced by the rotation of the Earth. On the rotating sphere, the sum of the force of the gravitational field and the centrifugal force yields an angular deviation of approximately

- - sin ⁡ ( 2 φ ) 2 g R Ω 2 {\displaystyle {\frac {\sin(2\varphi )}{2g}}{R\Omega ^{2}}}

(in radians) between the direction of the gravitational field and the direction measured by a plumb line; the plumb line appears to point southwards on the northern hemisphere and northwards on the southern hemisphere. Ω ≈ 7.29 × 10 − 5 {\displaystyle \Omega \approx 7.29\times 10^{-5}} rad/s is the diurnal angular speed of the Earth axis, and R ≈ 6370 {\displaystyle R\approx 6370} km the radius of the reference sphere, and R sin ⁡ φ {\displaystyle R\sin \varphi } the distance of the point on the Earth crust to the Earth axis. [3]

For the mass attraction effect by itself, the gravitational acceleration at the equator is about 0.18% less than that at the poles due to being located farther from the mass center. When the rotational component is included (as above), the gravity at the equator is about 0.53% less than that at the poles, with gravity at the poles being unaffected by the rotation. So the rotational component of change due to latitude (0.35%) is about twice as significant as the mass attraction change due to latitude (0.18%), but both reduce strength of gravity at the equator as compared to gravity at the poles.

Note that for satellites, orbits are decoupled from the rotation of the Earth so the orbital period is not necessarily one day, but also that errors can accumulate over multiple orbits so that accuracy is important. For such problems, the rotation of the Earth would be immaterial unless variations with longitude are modeled. Also, the variation in gravity with altitude becomes important, especially for highly elliptical orbits.

The *Earth Gravitational Model 1996* ([EGM96](/source/EGM96)) contains 130,676 coefficients that refine the model of the Earth's gravitational field.[2]: 40 The most significant correction term is about two orders of magnitude more significant than the next largest term.[2]: 40 That coefficient is referred to as the J 2 {\displaystyle J_{2}} term, and accounts for the flattening of the poles, or the [oblateness](/source/Oblate_spheroid), of the Earth. A gravitational potential function can be written for the change in potential energy for a unit mass that is brought from infinity into proximity to the Earth. Taking partial derivatives of that function with respect to a coordinate system will then resolve the directional components of the gravitational acceleration vector, as a function of location. The component due to the Earth's rotation can then be included, if appropriate, based on a [sidereal](/source/Sidereal_time) day relative to the stars (≈366.24 days/year) rather than on a [solar](/source/Solar_time) day (≈365.24 days/year). That component is perpendicular to the axis of rotation rather than to the surface of the Earth.

A similar model adjusted for the geometry and gravitational field for Mars can be found in publication NASA SP-8010.[4]

The [barycentric](/source/Center_of_mass) gravitational acceleration at a point in space is given by:

- g = − G M r 2 r ^ {\displaystyle \mathbf {g} =-{GM \over r^{2}}\mathbf {\hat {r}} }

where:

*M* is the mass of the attracting object, r ^ {\displaystyle \scriptstyle \mathbf {\hat {r}} } is the [unit vector](/source/Unit_vector) from center-of-mass of the attracting object to the center-of-mass of the object being accelerated, *r* is the distance between the two objects, and *G* is the [gravitational constant](/source/Gravitational_constant).

When this calculation is done for objects on the surface of the Earth, or aircraft that rotate with the Earth, one has to account for the fact that the Earth is rotating and the centrifugal acceleration has to be subtracted from this. For example, the equation above gives the acceleration at 9.820 m/s2, when *GM* = 3.986 × 1014 m3/s2, and *R* = 6.371 × 106 m. The centripetal radius is *r* = *R* cos(*φ*), and the centripetal time unit is approximately (*day* / 2*π*), reduces this, for *r* = 5 × 106 metres, to 9.79379 m/s2, which is closer to the observed value. [*[citation needed](https://en.wikipedia.org/wiki/Wikipedia:Citation_needed)*]

## Basic formulas

Various, successively more refined, formulas for computing the theoretical gravity are referred to as the *International Gravity Formula*, the first of which was proposed in 1930 by the [International Association of Geodesy](/source/International_Association_of_Geodesy). The general shape of that formula is:

- g ( ϕ ) = g e ( 1 + A sin 2 ⁡ ( ϕ ) − B sin 2 ⁡ ( 2 ϕ ) ) , {\displaystyle g(\phi )=g_{e}\left(1+A\sin ^{2}(\phi )-B\sin ^{2}(2\phi )\right),}

in which g(*φ*) is the gravity as a function of the [geographic latitude](/source/Geographic_latitude) *φ* of the position whose gravity is to be determined, g e {\displaystyle g_{e}} denotes the gravity at the equator (as determined by measurement), and the coefficients A and B are parameters that must be selected to produce a good global fit to true gravity.[5]

Using the values of the [GRS80](/source/GRS80) reference system, a commonly used specific instantiation of the formula above is given by:

- g ( ϕ ) = 9.780327 ( 1 + 0.0053024 sin 2 ⁡ ( ϕ ) − 0.0000058 sin 2 ⁡ ( 2 ϕ ) ) m s − 2 . {\displaystyle g(\phi )=9.780327\left(1+0.0053024\sin ^{2}(\phi )-0.0000058\sin ^{2}(2\phi )\right)\,\mathrm {ms} ^{-2}.} [5]

Using the appropriate [double-angle formula](/source/Double-angle_formula) in combination with the [Pythagorean identity](/source/Pythagorean_identity), this can be rewritten in the equivalent forms

- g ( ϕ ) = 9.780327 ( 1 + 0.0052792 sin 2 ⁡ ( ϕ ) + 0.0000232 sin 4 ⁡ ( ϕ ) ) m s − 2 , = 9.780327 ( 1.0053024 − .0053256 cos 2 ⁡ ( ϕ ) + .0000232 cos 4 ⁡ ( ϕ ) ) m s − 2 , = 9.780327 ( 1.0026454 − 0.0026512 cos ⁡ ( 2 ϕ ) + .0000058 cos 2 ⁡ ( 2 ϕ ) ) m s − 2 . {\displaystyle {\begin{aligned}g(\phi )&=9.780327\left(1+0.0052792\sin ^{2}(\phi )+0.0000232\sin ^{4}(\phi )\right)\,\mathrm {ms} ^{-2},\\&=9.780327\left(1.0053024-.0053256\cos ^{2}(\phi )+.0000232\cos ^{4}(\phi )\right)\,\mathrm {ms} ^{-2},\\&=9.780327\left(1.0026454-0.0026512\cos(2\phi )+.0000058\cos ^{2}(2\phi )\right)\,\mathrm {ms} ^{-2}.\end{aligned}}\,\!}

Up to the 1960s, formulas based on the [Hayford ellipsoid](/source/Hayford_ellipsoid) (1924) and of the famous German geodesist [Helmert](/source/Helmert) (1906) were often used.[*[citation needed](https://en.wikipedia.org/wiki/Wikipedia:Citation_needed)*] The difference between the semi-major axis (equatorial radius) of the Hayford ellipsoid and that of the modern [WGS84](/source/WGS84) ellipsoid is 251 m; for Helmert's ellipsoid it is only 63 m.

## Somigliana equation

See also: [Clairaut's theorem (gravity)](/source/Clairaut's_theorem_(gravity))

A more recent theoretical formula for gravity as a function of latitude is the International Gravity Formula 1980 (IGF80), also based on the GRS80 ellipsoid but now using the Somigliana equation (after [Carlo Somigliana](/source/Carlo_Somigliana) (1860–1955)[6]):

- g ( ϕ ) = g e [ 1 + k sin 2 ⁡ ( ϕ ) 1 − e 2 sin 2 ⁡ ( ϕ ) ] , {\displaystyle g(\phi )=g_{e}\left[{\frac {1+k\sin ^{2}(\phi )}{\sqrt {1-e^{2}\sin ^{2}(\phi )}}}\right],\,\!}

where,[7]

- k = b g p − a g e a g e {\displaystyle k={\frac {bg_{p}-ag_{e}}{ag_{e}}}} (formula constant);

- g e , g p {\displaystyle g_{e},g_{p}} is the defined gravity at the equator and poles, respectively;

- a , b {\displaystyle a,b} are the equatorial and polar semi-axes, respectively;

- e 2 = a 2 − b 2 a 2 {\displaystyle e^{2}={\frac {a^{2}-b^{2}}{a^{2}}}} is the spheroid's squared [eccentricity](/source/Eccentricity_(mathematics));

providing,

- g ( ϕ ) = 9.7803267715 [ 1 + 0.001931851353 sin 2 ⁡ ( ϕ ) 1 − 0.0066943800229 sin 2 ⁡ ( ϕ ) ] m s − 2 . {\displaystyle g(\phi )=9.7803267715\left[{\frac {1+0.001931851353\sin ^{2}(\phi )}{\sqrt {1-0.0066943800229\sin ^{2}(\phi )}}}\right]\,\mathrm {ms} ^{-2}.} [5]

A later refinement, based on the [WGS84](/source/WGS84) ellipsoid, is the WGS ([World Geodetic System](/source/World_Geodetic_System)) 1984 Ellipsoidal Gravity Formula:[7]

- g ( ϕ ) = 9.7803253359 [ 1 + 0.00193185265241 sin 2 ⁡ ( ϕ ) 1 − 0.00669437999013 sin 2 ⁡ ( ϕ ) ] m s − 2 . {\displaystyle g(\phi )=9.7803253359\left[{\frac {1+0.00193185265241\sin ^{2}(\phi )}{\sqrt {1-0.00669437999013\sin ^{2}(\phi )}}}\right]\,\mathrm {ms} ^{-2}.}

(where g p {\displaystyle g_{p}} = 9.8321849378 ms−2)

The difference with IGF80 is insignificant when used for [geophysical](/source/Geophysical) purposes,[5] but may be significant for other uses.

### Further details

For the normal gravity γ 0 {\displaystyle \gamma _{0}} of the sea level ellipsoid, i.e., elevation *h* = 0, this formula by Somigliana (1929) applies:

- γ 0 ( φ ) = a ⋅ γ a ⋅ cos 2 ⁡ φ + b ⋅ γ b ⋅ sin 2 ⁡ φ a 2 ⋅ cos 2 ⁡ φ + b 2 ⋅ sin 2 ⁡ φ {\displaystyle \gamma _{0}(\varphi )={\frac {a\cdot \gamma _{a}\cdot \cos ^{2}\varphi +b\cdot \gamma _{b}\cdot \sin ^{2}\varphi }{\sqrt {a^{2}\cdot \cos ^{2}\varphi +b^{2}\cdot \sin ^{2}\varphi }}}}

with

- γ a {\displaystyle \gamma _{a}} = Normal gravity at Equator

- γ b {\displaystyle \gamma _{b}} = Normal gravity at poles

- *a* = [semi-major axis](/source/Semi-major_and_semi-minor_axes) (Equator radius)

- *b* = [semi-minor axis](/source/Semi-major_and_semi-minor_axes) (pole radius)

- φ {\displaystyle \varphi } = [latitude](/source/Latitude)

Due to [numerical](/source/Numerical_analysis) issues, the formula is simplified to this:

- γ 0 ( φ ) = γ a ⋅ 1 + p ⋅ sin 2 ⁡ φ 1 − e 2 ⋅ sin 2 ⁡ φ {\displaystyle \gamma _{0}(\varphi )=\gamma _{a}\cdot {\frac {1+p\cdot \sin ^{2}\varphi }{\sqrt {1-e^{2}\cdot \sin ^{2}\varphi }}}}

with

- p = b ⋅ γ b a ⋅ γ a − 1 {\displaystyle p={\frac {b\cdot \gamma _{b}}{a\cdot \gamma _{a}}}-1}

- e 2 = 1 − b 2 a 2 ; {\displaystyle e^{2}=1-{\frac {b^{2}}{a^{2}}};\quad } (*e* is the [eccentricity](/source/Eccentricity_(mathematics)))

For the [Geodetic Reference System 1980 (GRS 80)](/source/GRS_80) the parameters are set to these values:

- a = 6 378 137 m b = 6 356 752 . 314 1 m {\displaystyle a=6\,378\,137\,\mathrm {m} \quad \quad \quad \quad b=6\,356\,752{.}314\,1\,\mathrm {m} }

- γ a = 9 . 780 326 771 5 m s 2 γ b = 9 . 832 186 368 5 m s 2 {\displaystyle \gamma _{a}=9{.}780\,326\,771\,5\,\mathrm {\frac {m}{s^{2}}} \quad \gamma _{b}=9{.}832\,186\,368\,5\,\mathrm {\frac {m}{s^{2}}} }

⇒ p = 1 . 931 851 353 ⋅ 10 − 3 e 2 = 6 . 694 380 022 90 ⋅ 10 − 3 {\displaystyle \Rightarrow p=1{.}931\,851\,353\cdot 10^{-3}\quad e^{2}=6{.}694\,380\,022\,90\cdot 10^{-3}}

## Approximation formula from series expansions

The Somigliana formula was approximated through different [series expansions](/source/Series_expansion), following this scheme:

- γ 0 ( φ ) = γ a ⋅ ( 1 + β ⋅ sin 2 ⁡ φ + β 1 ⋅ sin 2 ⁡ 2 φ + … ) {\displaystyle \gamma _{0}(\varphi )=\gamma _{a}\cdot (1+\beta \cdot \sin ^{2}\varphi +\beta _{1}\cdot \sin ^{2}2\varphi +\dots )}

### International gravity formula 1930

The normal gravity formula by [Gino Cassinis](/source/Gino_Cassinis) was determined in 1930 by [International Union of Geodesy and Geophysics](/source/International_Union_of_Geodesy_and_Geophysics) as international gravity formula along with [Hayford ellipsoid](/source/Hayford_ellipsoid). The parameters are:

- γ a = 9 . 78049 m s 2 β = 5 . 2884 ⋅ 10 − 3 β 1 = − 5 . 9 ⋅ 10 − 6 {\displaystyle \gamma _{a}=9{.}78049{\frac {\mathrm {m} }{\mathrm {s} ^{2}}}\quad \beta =5{.}2884\cdot 10^{-3}\quad \beta _{1}=-5{.}9\cdot 10^{-6}}

In the course of time the values were improved again with newer knowledge and more exact measurement methods.

[Harold Jeffreys](/source/Harold_Jeffreys) improved the values in 1948 at:

- γ a = 9 . 780373 m s 2 β = 5 . 2891 ⋅ 10 − 3 β 1 = − 5 . 9 ⋅ 10 − 6 {\displaystyle \gamma _{a}=9{.}780373{\frac {\mathrm {m} }{\mathrm {s} ^{2}}}\quad \beta =5{.}2891\cdot 10^{-3}\quad \beta _{1}=-5{.}9\cdot 10^{-6}}

### International gravity formula 1967

The normal gravity formula of Geodetic Reference System 1967 is defined with the values:

- γ a = 9 . 780318 m s 2 β = 5 . 3024 ⋅ 10 − 3 β 1 = − 5 . 9 ⋅ 10 − 6 {\displaystyle \gamma _{a}=9{.}780318{\frac {\mathrm {m} }{\mathrm {s} ^{2}}}\quad \beta =5{.}3024\cdot 10^{-3}\quad \beta _{1}=-5{.}9\cdot 10^{-6}}

### International gravity formula 1980

From the parameters of GRS 80 comes the classic series expansion:

- γ a = 9 . 780327 m s 2 β = 5 . 3024 ⋅ 10 − 3 β 1 = − 5 . 8 ⋅ 10 − 6 {\displaystyle \gamma _{a}=9{.}780327{\frac {\mathrm {m} }{\mathrm {s} ^{2}}}\quad \beta =5{.}3024\cdot 10^{-3}\quad \beta _{1}=-5{.}8\cdot 10^{-6}}

The accuracy is about ±10−6 m/s2.

With GRS 80 the following series expansion is also introduced:

- γ 0 ( φ ) = γ a ⋅ ( 1 + c 1 ⋅ sin 2 ⁡ φ + c 2 ⋅ sin 4 ⁡ φ + c 3 ⋅ sin 6 ⁡ φ + c 4 ⋅ sin 8 ⁡ φ + … ) {\displaystyle \gamma _{0}(\varphi )=\gamma _{a}\cdot (1+c_{1}\cdot \sin ^{2}\varphi +c_{2}\cdot \sin ^{4}\varphi +c_{3}\cdot \sin ^{6}\varphi +c_{4}\cdot \sin ^{8}\varphi +\dots )}

As such the parameters are:

- *c*1 = 5.279 0414·10−3

- *c*2 = 2.327 18·10−5

- *c*3 = 1.262·10−7

- *c*4 = 7·10−10

The accuracy is at about ±10−9 m/s2 exact. When the exactness is not required, the terms at further back can be omitted. But it is recommended to use this finalized formula.

## Height dependence

Cassinis determined the height dependence, as:

- g ( φ , h ) = g 0 ( φ ) − ( 3 . 08 ⋅ 10 − 6 1 s 2 − 4 . 19 ⋅ 10 − 7 c m 3 g ⋅ s 2 ⋅ ρ ) ⋅ h {\displaystyle g(\varphi ,h)=g_{0}(\varphi )-\left(3{.}08\cdot 10^{-6}\,{\frac {1}{\mathrm {s} ^{2}}}-4{.}19\cdot 10^{-7}\,{\frac {\mathrm {cm} ^{3}}{\mathrm {g} \cdot \mathrm {s} ^{2}}}\cdot \rho \right)\cdot h}

The average rock [density](/source/Density) ρ is no longer considered.

Since GRS 1967 the dependence on the [ellipsoidal elevation](/source/Elevation) *h* is:

- g ( φ , h ) = g 0 ( φ ) − ( 1 − 1 . 39 ⋅ 10 − 3 ⋅ sin 2 ⁡ ( φ ) ) ⋅ 3 . 0877 ⋅ 10 − 6 1 s 2 ⋅ h + 7 . 2 ⋅ 10 − 13 1 m ⋅ s 2 ⋅ h 2 = g 0 ( φ ) − ( 3 . 0877 ⋅ 10 − 6 − 4 . 3 ⋅ 10 − 9 ⋅ sin 2 ⁡ ( φ ) ) 1 s 2 ⋅ h + 7 . 2 ⋅ 10 − 13 1 m ⋅ s 2 ⋅ h 2 {\displaystyle {\begin{aligned}g(\varphi ,h)&=g_{0}(\varphi )-\left(1-1{.}39\cdot 10^{-3}\cdot \sin ^{2}(\varphi )\right)\cdot 3{.}0877\cdot 10^{-6}\,{\frac {1}{\mathrm {s} ^{2}}}\cdot h+7{.}2\cdot 10^{-13}\,{\frac {1}{\mathrm {m} \cdot \mathrm {s} ^{2}}}\cdot h^{2}\\&=g_{0}(\varphi )-\left(3{.}0877\cdot 10^{-6}-4{.}3\cdot 10^{-9}\cdot \sin ^{2}(\varphi )\right)\,{\frac {1}{\mathrm {s} ^{2}}}\cdot h+7{.}2\cdot 10^{-13}\,{\frac {1}{\mathrm {m} \cdot \mathrm {s} ^{2}}}\cdot h^{2}\end{aligned}}}

Another expression is:

- g ( φ , h ) = g 0 ( φ ) ⋅ ( 1 − ( k 1 − k 2 ⋅ sin 2 ⁡ φ ) ⋅ h + k 3 ⋅ h 2 ) {\displaystyle g(\varphi ,h)=g_{0}(\varphi )\cdot (1-(k_{1}-k_{2}\cdot \sin ^{2}\varphi )\cdot h+k_{3}\cdot h^{2})}

with the parameters derived from GRS80:

- k 1 = 2 ⋅ ( 1 + f + m ) / a = 3 . 157 04 ⋅ 10 − 7 m − 1 {\displaystyle k_{1}=2\cdot (1+f+m)/a=3{.}157\,04\cdot 10^{-7}\,\mathrm {m^{-1}} }

- k 2 = 4 ⋅ f / a = 2 . 102 69 ⋅ 10 − 9 m − 1 {\displaystyle k_{2}=4\cdot f/a=2{.}102\,69\cdot 10^{-9}\,\mathrm {m^{-1}} }

- k 3 = 3 / ( a 2 ) = 7 . 374 52 ⋅ 10 − 14 m − 2 {\displaystyle k_{3}=3/(a^{2})=7{.}374\,52\cdot 10^{-14}\,\mathrm {m^{-2}} }

where m {\displaystyle m} with ω = 7.2921150 ⋅ 10 − 5 r a d ⋅ s − 1 {\displaystyle \omega =7.2921150\cdot 10^{-5}\ rad\cdot s^{-1}} :[8]

- m = ω 2 ⋅ a 2 ⋅ b G M {\displaystyle m={\frac {\omega ^{2}\cdot a^{2}\cdot b}{GM}}}

This adjustment is about right for common heights in [aviation](/source/Aviation); but for heights up to [outer space](/source/Outer_space) (over ca. 100 kilometers) it is [out of range](/source/Limit_of_a_function).

## WELMEC formula

In all German [standards offices](/source/Standards_organization) the free-fall acceleration *g* is calculated in respect to the average latitude φ and the average [height above sea level](/source/Sea_level) *h* with the [WELMEC](/source/WELMEC)–Formel:

- g ( φ , h ) = ( 1 + 0 . 0053024 ⋅ sin 2 ⁡ ( φ ) − 0 . 0000058 ⋅ sin 2 ⁡ ( 2 φ ) ) ⋅ 9 . 780318 m s 2 − 0 . 000003085 1 s 2 ⋅ h {\displaystyle g(\varphi ,h)=\left(1+0{.}0053024\cdot \sin ^{2}(\varphi )-0{.}0000058\cdot \sin ^{2}(2\varphi )\right)\cdot 9{.}780318{\frac {\mathrm {m} }{\mathrm {s} ^{2}}}-0{.}000003085\,{\frac {1}{\mathrm {s} ^{2}}}\cdot h}

The formula is based on the International gravity formula from 1967.

The scale of free-fall acceleration at a certain place must be determined with precision measurement of several mechanical magnitudes. [Weighing scales](/source/Weighing_scale), the mass of which does measurement because of the weight, relies on the free-fall acceleration, thus for use they must be prepared with different constants in different places of use. Through the concept of so-called gravity zones, which are divided with the use of normal gravity, a weighing scale can be calibrated by the manufacturer before use.[9]

## Example

*[Free-fall acceleration](/source/Free_fall) in [Schweinfurt](/source/Schweinfurt):*

*Data:*

- Latitude: 50° 3′ 24″ = 50.0567°

- Height above sea level: 229.7 m

- Density of the rock plates: ca. 2.6 g/cm3

- Measured free-fall acceleration: g = 9.8100 ± 0.0001 m/s2

*Free-fall acceleration, calculated through normal gravity formulas:*

- Cassinis: *g* = 9.81038 m/s2

- Jeffreys: *g* = 9.81027 m/s2

- WELMEC: *g* = 9.81004 m/s2

## See also

- [Gravity anomaly](/source/Gravity_anomaly)

- [Reference ellipsoid](/source/Reference_ellipsoid)

- [EGM96](/source/EGM96) (Earth Gravitational Model 1996)

- [Standard gravity](/source/Standard_gravity) : 9.806 65 m/s2

## References

1. **[^](#cite_ref-1)** Izzo, Dario; Gómez, Pablo (2022-12-28). ["Geodesy of irregular small bodies via neural density fields"](https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10956048). *Communications Engineering*. **1** (1): 48. [arXiv](/source/ArXiv_(identifier)):[2105.13031](https://arxiv.org/abs/2105.13031). [Bibcode](/source/Bibcode_(identifier)):[2022CmEng...1...48I](https://ui.adsabs.harvard.edu/abs/2022CmEng...1...48I). [doi](/source/Doi_(identifier)):[10.1038/s44172-022-00050-3](https://doi.org/10.1038%2Fs44172-022-00050-3). [ISSN](/source/ISSN_(identifier)) [2731-3395](https://search.worldcat.org/issn/2731-3395). [PMC](/source/PMC_(identifier)) [10956048](https://www.ncbi.nlm.nih.gov/pmc/articles/PMC10956048).

1. ^ [***a***](#cite_ref-Stevens&Lewis_2-0) [***b***](#cite_ref-Stevens&Lewis_2-1) [***c***](#cite_ref-Stevens&Lewis_2-2) [***d***](#cite_ref-Stevens&Lewis_2-3) Brian L. Stevens; Frank L. Lewis (2003). *Aircraft Control And Simulation, 2nd Ed*. Hoboken, New Jersey: [John Wiley & Sons, Inc.](/source/John_Wiley_%26_Sons%2C_Inc.) [ISBN](/source/ISBN_(identifier)) [978-0-471-37145-8](https://en.wikipedia.org/wiki/Special:BookSources/978-0-471-37145-8).

1. **[^](#cite_ref-3)** de Icaza-Herrera, M.; Castano, V. M. (2011). "Generalized Lagrangian of the parametric Foucault pendulum with dissipative forces". *Acta Mech*. **218** (1–2): 45–64. [doi](/source/Doi_(identifier)):[10.1007/s00707-010-0392-8](https://doi.org/10.1007%2Fs00707-010-0392-8).

1. **[^](#cite_ref-SP8010_4-0)** Richard B. Noll; Michael B. McElroy (1974), "Models of Mars' Atmosphere [1974]", *Space Vehicle Design Criteria (Environment)*, Greenbelt, Maryland: NASA Goddard Space Flight Center, [Bibcode](/source/Bibcode_(identifier)):[1974svdc.rept......](https://ui.adsabs.harvard.edu/abs/1974svdc.rept......), SP-8010.

1. ^ [***a***](#cite_ref-GaME_5-0) [***b***](#cite_ref-GaME_5-1) [***c***](#cite_ref-GaME_5-2) [***d***](#cite_ref-GaME_5-3) William J. Hinze; [Ralph R. B. von Frese](/source/Ralph_von_Frese); Afif H. Saad (2013). *Gravity and Magnetic Exploration: Principles, Practices, and Applications*. [Cambridge University Press](/source/Cambridge_University_Press). p. 130. [ISBN](/source/ISBN_(identifier)) [978-1-107-32819-8](https://en.wikipedia.org/wiki/Special:BookSources/978-1-107-32819-8).

1. **[^](#cite_ref-6)** [Biografie Somiglianas](http://www.torinoscienza.it/accademia/personaggi/carlo_somigliana_20033) [Archived](https://web.archive.org/web/20101207145309/http://www.torinoscienza.it/accademia/personaggi/carlo_somigliana_20033) 2010-12-07 at the [Wayback Machine](/source/Wayback_Machine) (ital.)

1. ^ [***a***](#cite_ref-DoD-WGS84_7-0) [***b***](#cite_ref-DoD-WGS84_7-1) [***Department of Defense World Geodetic System 1984 — Its Definition and Relationships with Local Geodetic Systems***,NIMA TR8350.2, 3rd ed., Tbl. 3.4, Eq. 4-1](http://earth-info.nga.mil/GandG/publications/tr8350.2/wgs84fin.pdf)

1. **[^](#cite_ref-8)** Xiong Li; Hans-Jürgen Götzez. ["Tutorial: Ellipsoid, geoid, gravity, geodesy, and geophysics"](https://geored2.sgc.gov.co/Articulos%20y%20documentacion/Li_G_Tut.pdf) (PDF). Retrieved 29 March 2024.{{[cite web](https://en.wikipedia.org/wiki/Template:Cite_web)}}: CS1 maint: multiple names: authors list ([link](https://en.wikipedia.org/wiki/Category:CS1_maint:_multiple_names:_authors_list)) 988kB

1. **[^](#cite_ref-9)** Roman Schwartz, Andreas Lindau. ["Das europäische Gravitationszonenkonzept nach WELMEC"](http://www.ptb.de/de/org/1/11/115/doc/gravzonen.pdf) (PDF) (in German). Retrieved 26 February 2011. 700kB

## Further reading

- [Karl Ledersteger](/source/Karl_Ledersteger): *Astronomische und [physikalische Geodäsie](/source/Physical_geodesy)*. Handbuch der Vermessungskunde Band 5, 10. Auflage. Metzler, Stuttgart 1969

- B.Hofmann-Wellenhof, [Helmut Moritz](/source/Helmut_Moritz): *Physical Geodesy*, [ISBN](/source/ISBN_(identifier)) [3-211-23584-1](https://en.wikipedia.org/wiki/Special:BookSources/3-211-23584-1), Springer-Verlag Wien 2006.

- [Wolfgang Torge](https://en.wikipedia.org/w/index.php?title=Wolfgang_Torge&action=edit&redlink=1): *Geodäsie*. 2. Auflage. Walter de Gruyter, Berlin u.a. 2003. [ISBN](/source/ISBN_(identifier)) [3-11-017545-2](https://en.wikipedia.org/wiki/Special:BookSources/3-11-017545-2)

- [Wolfgang Torge](https://en.wikipedia.org/w/index.php?title=Wolfgang_Torge&action=edit&redlink=1): *Geodäsie*. Walter de Gruyter, Berlin u.a. 1975 [ISBN](/source/ISBN_(identifier)) [3-11-004394-7](https://en.wikipedia.org/wiki/Special:BookSources/3-11-004394-7)

## External links

- *[Definition des Geodetic Reference System 1980 (GRS80)](http://www.bkg.bund.de/nn_164850/geodIS/EVRS/EN/References/Definitions/Def__GRS80-pdf,templateId=raw,property=publicationFile.pdf/Def_GRS80-pdf.pdf)* (pdf, engl.; 70 kB)

- [Gravity Information System](http://www.ptb.de/cartoweb3/SISproject.php) der [Physikalisch-Technischen Bundesanstalt](/source/Physikalisch-Technische_Bundesanstalt), engl.

- [Online-Berechnung der Normalschwere mit verschiedenen Normalschwereformeln](http://www.in-dubio-pro-geo.de/index.php?file=ellip/ngrav0)

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Adapted from the Wikipedia article [Theoretical gravity](https://en.wikipedia.org/wiki/Theoretical_gravity) by Wikipedia contributors ([contributor history](https://en.wikipedia.org/wiki/Theoretical_gravity?action=history)). Available under [Creative Commons Attribution-ShareAlike 4.0 International](https://creativecommons.org/licenses/by-sa/4.0/). Changes may have been made.