# Difference between revisions of "Gravitational acceleration"

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+ | {{main|Classical mechanics}} | ||

{{refimprove|date=December 2010}} | {{refimprove|date=December 2010}} | ||

− | In [[physics]], '''gravitational acceleration''' is the [[acceleration]] on an object caused by [[ | + | In [[physics]], '''gravitational acceleration''' is the [[acceleration]] on an object caused by force of [[gravitation]]. Neglecting friction such as air resistance, all small bodies accelerate in a [[gravitational field]] at the same rate relative to the center of mass.<ref> |

{{cite book | {{cite book | ||

| title = Physics, the human adventure: from Copernicus to Einstein and beyond | | title = Physics, the human adventure: from Copernicus to Einstein and beyond | ||

Line 11: | Line 12: | ||

| page = 113 | | page = 113 | ||

| url = http://books.google.com/books?id=czaGZzR0XOUC&pg=PA113&dq=%22gravitational+acceleration%22+%22all+objects%22+neglecting+air&hl=en&ei=KSb8TIDVIofGsAOUsNX2DQ&sa=X&oi=book_result&ct=result&resnum=1&ved=0CCgQ6AEwAA#v=onepage&q=%22gravitational%20acceleration%22%20%22all%20objects%22%20neglecting%20air&f=false | | url = http://books.google.com/books?id=czaGZzR0XOUC&pg=PA113&dq=%22gravitational+acceleration%22+%22all+objects%22+neglecting+air&hl=en&ei=KSb8TIDVIofGsAOUsNX2DQ&sa=X&oi=book_result&ct=result&resnum=1&ved=0CCgQ6AEwAA#v=onepage&q=%22gravitational%20acceleration%22%20%22all%20objects%22%20neglecting%20air&f=false | ||

− | }}</ref> | + | }}</ref> This equality is true regardless of the masses or compositions of the bodies. |

+ | |||

+ | At different points on Earth, objects fall with an acceleration between 9.78 and 9.82 m/s<sup>2</sup> depending on [[altitude]], with a [[convention (norm)|conventional]] [[standard gravity|standard value]] of exactly 9.80665 m/s<sup>2</sup> (approx. 32.174 ft/s<sup>2</sup>). Objects with low densities do not accelerate as rapidly due to [[buoyancy]] and air resistance. | ||

+ | |||

+ | == For point masses == | ||

+ | |||

+ | |||

+ | Newton's [[Law of Universal Gravitation]] states that there is a gravitational force between any two masses that is equal in magnitude for each mass, and is aligned to draw the two masses toward each other. The formula is: | ||

+ | |||

+ | :<math>F = G \frac{m_1 m_2}{r^2}\ </math> | ||

+ | |||

+ | where <math>m_1</math> and <math>m_2</math> are the two masses, <math>G</math> is the [[gravitational constant]], and <math>r</math> is the distance between the two masses. The formula was derived for planetary motion where the distances between the planets and the Sun made it reasonable to consider the bodies to be point masses. (For a satellite in orbit, the 'distance' refers to the distance from the mass centers rather than, say, the altitude above a planet's surface.) | ||

+ | |||

+ | If one of the masses is much larger than the other, it is convenient to define a gravitational field around the larger mass as follows:<ref name=Bueche> | ||

+ | {{cite book | ||

+ | | author = [[Fredrick J. Bueche]] | ||

+ | | title = Introduction to Physics for Scientists and Engineers, 2nd Ed. | ||

+ | | year = 1975 | ||

+ | | publisher = Von Hoffmann Press | ||

+ | | location = USA | ||

+ | | ISBN = 0-07-008836-5 | ||

+ | }}</ref> | ||

+ | |||

+ | :<math>\mathbf{g}=- {G M \over r^2}\mathbf{\hat{r}}</math> | ||

+ | |||

+ | where <math>M</math> is the mass of the larger body, and <math>\mathbf{\hat{r}}</math> is a unit vector directed from the large mass to the smaller mass. The negative sign indicates that the force is an attractive force. | ||

+ | |||

+ | In that way, the force acting upon the smaller mass can be calculated as: | ||

+ | |||

+ | :<math>\mathbf{F} = m \mathbf{g}</math> | ||

+ | |||

+ | where <math>\mathbf{F}</math> is the force vector, <math>m</math> is the smaller mass, and <math>\mathbf{g}</math> is a vector pointed toward the larger body. Note that <math>\mathbf{g}</math> has units of acceleration and is a vector function of location relative to the large body, independent of the magnitude (or even the presence) of the smaller mass. | ||

+ | |||

+ | This model represents the "far-field" gravitational acceleration associated with a massive body. When the dimensions of a body are not trivial compared to the distances of interest, the principle of superposition can be used for differential masses for an assumed density distribution throughout the body in order to get a more detailed model of the "near-field" gravitational acceleration. For satellites in orbit, the far-field model is sufficient for rough calculations of altitude versus period, but not for precision estimation of future location after multiple orbits. | ||

− | + | The more detailed models include (among other things) the bulging at the equator for the Earth, and irregular mass concentrations (due to meteor impacts) for the Moon. The ''Gravity Recovery And Climate Experiment'' ([[Gravity Recovery and Climate Experiment|GRACE]]) mission launched in 2002 consists of two probes, nicknamed "Tom" and "Jerry", in polar orbit around the Earth measuring differences in the distance between the two probes in order to more precisely determine the gravitational field around the Earth, and to track changes that occur over time. Similarly, the ''Gravity Recovery and Interior Laboratory'' ([[Gravity Recovery and Interior Laboratory|GRAIL]]) mission from 2011-2012 consisted of two probes ("Ebb" and "Flow") in polar orbit around the Moon to more precisely determine the gravitational field for future navigational purposes, and to infer information about the Moon's physical makeup. | |

− | == | + | == Gravity model for Earth == |

+ | 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:<ref name=Stevens&Lewis> | ||

+ | {{cite book | ||

+ | | author1=Brian L. Stevens | ||

+ | | author2=Frank L. Lewis | ||

+ | | title=Aircraft Control And Simulation, 2nd Ed. | ||

+ | | year=2003 | ||

+ | | publisher=John Wiley & Sons, Inc. | ||

+ | | location=Hoboken, New Jersey | ||

+ | | ISBN = 0-471-37145-9 | ||

+ | }}</ref> | ||

− | {{ | + | :<math>\mathbf{g}=</math> <big>{{convert|9.80665|m|ft}} per s²</big> |

+ | |||

+ | based upon data from ''World Geodetic System 1984'' ([[World Geodetic System|WGS-84]]), where <math>\mathbf{g}</math> 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, one could use the following (,<ref name=Stevens&Lewis/> p. 41): | ||

+ | |||

+ | :<math>\mathbf{g}=G_{45} - (G_{poles}-G_{equator})\cdot \cos\left(2\cdot lat\cdot \frac{\pi}{180}\right)</math> | ||

+ | |||

+ | where | ||

+ | * <math>G_{poles}</math> = {{convert|9.832|m|ft}} per s² | ||

+ | * <math>G_{45}</math> = {{convert|9.806|m|ft}} per s² | ||

+ | * <math>G_{equator}</math> = {{convert|9.780|m|ft}} per s² | ||

+ | * ''lat'' = latitude, between −90 and 90 degrees | ||

+ | |||

+ | Both these models take into account the centrifugal relief that is produced by the rotation of the Earth, and neither accounts for changes in gravity with changes in altitude. It is worth noting that 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 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]]) contains 130,676 coefficients that refine the model of the Earth's gravitational field (,<ref name=Stevens&Lewis/> p. 40). The most significant correction term is about two orders of magnitude more significant than the next largest term (,<ref name=Stevens&Lewis/> p. 40). That coefficient is referred to as the <math>J_2</math> term, and accounts for the flattening of the poles, or the [[oblate spheroid|oblateness]], of the Earth. (A shape elongated on its axis-of-symmetry, like an American football, would be called [[prolate]].) 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 time|sidereal]] day relative to the stars (≈366.24 days/year) rather than on a [[solar time|solar]] 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.<ref name=SP8010> | ||

+ | {{citation | ||

+ | | author1=Richard B. Noll | ||

+ | | author2=Michael B. McElroy | ||

+ | | title=Models of Mars' Atmosphere [1974] | ||

+ | | year=1974 | ||

+ | | publisher=NASA Goddard Space Flight Center | ||

+ | | location=Greenbelt, Maryland | ||

+ | | id=SP-8010. | ||

+ | }}</ref> | ||

The [[Center of mass|barycentric]] gravitational acceleration at a point in space is given by: | The [[Center of mass|barycentric]] gravitational acceleration at a point in space is given by: | ||

− | :<math>\mathbf | + | :<math>\mathbf{g}=-{G M \over r^2}\mathbf{\hat{r}}</math> |

where: | where: | ||

− | ''M'' is the mass of the attracting object, <math>\scriptstyle \mathbf{\hat{r}}</math> is the [[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]]. | + | ''M'' is the mass of the attracting object, <math>\scriptstyle \mathbf{\hat{r}}</math> is the [[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]]. |

− | |||

− | |||

− | + | When this calculation is done for objects on the surface of the Earth, or aircraft that rotate with the Earth, one has to account 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 = 3.986E14 m³/s², and R=6.371E6 m. The centripetal radius is r = R cos(latitude), and the centripetal time unit is approximately (day / 2pi), reduces this for r = 5E6 metres, to 9.79379 m/s², which is closer to the observed value. | |

− | + | Disregarding air resistance, all small masses dropped simultaneously from the same height will hit the ground at the same time; for example, during [[Apollo 15]] an astronaut on the Moon simultaneously dropped a feather and a hammer and they reached the ground at the same time. | |

− | |||

− | |||

==General relativity== | ==General relativity== | ||

Line 39: | Line 108: | ||

In Einstein's theory of [[general relativity]], gravitation is an attribute of curved [[spacetime]] instead of being due to a force propagated between bodies. In Einstein's theory, masses distort spacetime in their vicinity, and other particles move in trajectories determined by the geometry of spacetime. The gravitational force is a [[Fictitious force#Gravity as a fictitious force|fictitious force]]. There is no gravitational acceleration, in that the [[proper acceleration]] and hence [[four-acceleration]] of objects in [[free fall]] are zero. Rather than undergoing an acceleration, objects in free fall travel along straight lines ([[Geodesic (general relativity)|geodesics]]) on the curved spacetime. | In Einstein's theory of [[general relativity]], gravitation is an attribute of curved [[spacetime]] instead of being due to a force propagated between bodies. In Einstein's theory, masses distort spacetime in their vicinity, and other particles move in trajectories determined by the geometry of spacetime. The gravitational force is a [[Fictitious force#Gravity as a fictitious force|fictitious force]]. There is no gravitational acceleration, in that the [[proper acceleration]] and hence [[four-acceleration]] of objects in [[free fall]] are zero. Rather than undergoing an acceleration, objects in free fall travel along straight lines ([[Geodesic (general relativity)|geodesics]]) on the curved spacetime. | ||

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==See also== | ==See also== | ||

+ | *[[Air track]] | ||

+ | *[[Gravimetry]] | ||

+ | *[[Gravity of Earth]] | ||

*[[Newton's law of universal gravitation]] | *[[Newton's law of universal gravitation]] | ||

− | |||

*[[Standard gravity]] | *[[Standard gravity]] | ||

− | + | ||

− | + | == References == | |

+ | |||

+ | {{reflist}} | ||

{{DEFAULTSORT:Gravitational Acceleration}} | {{DEFAULTSORT:Gravitational Acceleration}} | ||

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[[Category:Gravitation]] | [[Category:Gravitation]] | ||

[[Category:Acceleration]] | [[Category:Acceleration]] | ||

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## Revision as of 20:36, 23 October 2013

{{#invoke:main|main}} {{ safesubst:#invoke:Unsubst||$N=Refimprove |date=__DATE__ |$B= {{#invoke:Message box|ambox}} }}

In physics, **gravitational acceleration** is the acceleration on an object caused by force of gravitation. Neglecting friction such as air resistance, all small bodies accelerate in a gravitational field at the same rate relative to the center of mass.^{[1]} This equality is true regardless of the masses or compositions of the bodies.

At different points on Earth, objects fall with an acceleration between 9.78 and 9.82 m/s^{2} depending on altitude, with a conventional standard value of exactly 9.80665 m/s^{2} (approx. 32.174 ft/s^{2}). Objects with low densities do not accelerate as rapidly due to buoyancy and air resistance.

## For point masses

Newton's Law of Universal Gravitation states that there is a gravitational force between any two masses that is equal in magnitude for each mass, and is aligned to draw the two masses toward each other. The formula is:

where and are the two masses, is the gravitational constant, and is the distance between the two masses. The formula was derived for planetary motion where the distances between the planets and the Sun made it reasonable to consider the bodies to be point masses. (For a satellite in orbit, the 'distance' refers to the distance from the mass centers rather than, say, the altitude above a planet's surface.)

If one of the masses is much larger than the other, it is convenient to define a gravitational field around the larger mass as follows:^{[2]}

where is the mass of the larger body, and is a unit vector directed from the large mass to the smaller mass. The negative sign indicates that the force is an attractive force.

In that way, the force acting upon the smaller mass can be calculated as:

where is the force vector, is the smaller mass, and is a vector pointed toward the larger body. Note that has units of acceleration and is a vector function of location relative to the large body, independent of the magnitude (or even the presence) of the smaller mass.

This model represents the "far-field" gravitational acceleration associated with a massive body. When the dimensions of a body are not trivial compared to the distances of interest, the principle of superposition can be used for differential masses for an assumed density distribution throughout the body in order to get a more detailed model of the "near-field" gravitational acceleration. For satellites in orbit, the far-field model is sufficient for rough calculations of altitude versus period, but not for precision estimation of future location after multiple orbits.

The more detailed models include (among other things) the bulging at the equator for the Earth, and irregular mass concentrations (due to meteor impacts) for the Moon. The *Gravity Recovery And Climate Experiment* (GRACE) mission launched in 2002 consists of two probes, nicknamed "Tom" and "Jerry", in polar orbit around the Earth measuring differences in the distance between the two probes in order to more precisely determine the gravitational field around the Earth, and to track changes that occur over time. Similarly, the *Gravity Recovery and Interior Laboratory* (GRAIL) mission from 2011-2012 consisted of two probes ("Ebb" and "Flow") in polar orbit around the Moon to more precisely determine the gravitational field for future navigational purposes, and to infer information about the Moon's physical makeup.

## Gravity model for Earth

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:^{[3]}

- Template:Convert per s²

based upon data from *World Geodetic System 1984* (WGS-84), where 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, one could use the following (,^{[3]} p. 41):

where

- = Template:Convert per s²
- = Template:Convert per s²
- = Template:Convert per s²
*lat*= latitude, between −90 and 90 degrees

Both these models take into account the centrifugal relief that is produced by the rotation of the Earth, and neither accounts for changes in gravity with changes in altitude. It is worth noting that 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 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) contains 130,676 coefficients that refine the model of the Earth's gravitational field (,^{[3]} p. 40). The most significant correction term is about two orders of magnitude more significant than the next largest term (,^{[3]} p. 40). That coefficient is referred to as the term, and accounts for the flattening of the poles, or the oblateness, of the Earth. (A shape elongated on its axis-of-symmetry, like an American football, would be called prolate.) 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 day relative to the stars (≈366.24 days/year) rather than on a solar 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 gravitational acceleration at a point in space is given by:

where:

*M* is the mass of the attracting object, is the 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.

When this calculation is done for objects on the surface of the Earth, or aircraft that rotate with the Earth, one has to account 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 = 3.986E14 m³/s², and R=6.371E6 m. The centripetal radius is r = R cos(latitude), and the centripetal time unit is approximately (day / 2pi), reduces this for r = 5E6 metres, to 9.79379 m/s², which is closer to the observed value.

Disregarding air resistance, all small masses dropped simultaneously from the same height will hit the ground at the same time; for example, during Apollo 15 an astronaut on the Moon simultaneously dropped a feather and a hammer and they reached the ground at the same time.

## General relativity

{{#invoke:main|main}}

In Einstein's theory of general relativity, gravitation is an attribute of curved spacetime instead of being due to a force propagated between bodies. In Einstein's theory, masses distort spacetime in their vicinity, and other particles move in trajectories determined by the geometry of spacetime. The gravitational force is a fictitious force. There is no gravitational acceleration, in that the proper acceleration and hence four-acceleration of objects in free fall are zero. Rather than undergoing an acceleration, objects in free fall travel along straight lines (geodesics) on the curved spacetime.