gravity summary

19
Gravity Summary For a point source or for a homogeneous sphere the solution is easy to compute and are given by the Newton’s law. Gravity Force for the attraction of 2 point masses: F = G M 1 M 2 / R 2 a = GM / R 2 2 V = 0 outside the body and 2 V = - 4 π G inside the body Potential V = F (for unit mass thus g)

Upload: elvis

Post on 12-Jan-2016

26 views

Category:

Documents


4 download

DESCRIPTION

Gravity Summary. For a point source or for a homogeneous sphere the solution is easy to compute and are given by the Newton’s law. Gravity Force for the attraction of 2 point masses: F = G M 1 M 2 / R 2 a = GM / R 2  2 V = 0 outside the body and 2 V = - 4 π G  inside the body - PowerPoint PPT Presentation

TRANSCRIPT

Page 1: Gravity Summary

Gravity Summary

For a point source or for a homogeneous sphere the solution is easy to compute and are given by the Newton’s law.

Gravity Force for the attraction of 2 point masses:

F = G M1 M2 / R2

a = GM / R2

2 V = 0 outside the body and

2 V = - 4 π G inside the body

Potential V = F (for unit mass thus g)

Page 2: Gravity Summary

Gravity Summary

This kind of forces and potential are typical for conservative field and follow the same rules that you have seen for the Electric field. In particular:

2 V = 0 outside the body and

2 V = - 4 π G inside the body.

Are called Laplace and Poisson equations and are well known equations. The solution of the first equation are called harmonics.

Page 3: Gravity Summary

Gravity Summary

A general solution for the laplace problem can be written in spherical harmonics:

V=(GM/r) n=0∞ m=0

n (R/r)n (Cnm cos m + Snm sin m) Pnm (sin )

latitude, longitude, R Earth Radius, r distance from CM

The coefficient Cnm and Snm are called Stokes Coefficients.

Pnm(sin ) are associated Legendre functions

Ynm (,) = (Cnm cos m + Snm sin m) Pnm (sin )Is called spherical harmonics of degree n order m

Page 4: Gravity Summary

In generalCnm cos m Pnm (sin ) and Snm sin m Pnm (sin )

Are ortogonal functions =>each function for a given degree and ordercan be thought of as contributing independent information with an amplitude givenby their respective Cnm and Snm coefficients

The zonal harmonics corresponding to m=0 have no longitude dependence and have n zeroes between +- 90 degrees in latitude So the even degree zonals are symmetric about the equator and the odd zonal are asymmetric.Note also that as the degree increases the number of zeroes in latitude increases and the harmonics represent finer latitudinal variations in the potential. If only large scale, such as the bulge, need to be modeled, then only the lowest degree zonal terms need to be used.

Page 5: Gravity Summary

The non zonal harmonics have longitudinal variations.The presence of theCos m and sin m give the functions m zeroes in longitude And the Associated Legendre Functions have m zeroes in latitude. So similar to the zonals the higher degree and order harmonics represent finner spatial detail of the gravitational potential The non zonal coefficients are called tesserals and for the specic case of n=m they are referred to as sectorials.

Generally the spherical harmonics can be thought of as representing variations in the gravitational potential that have wavelengths of the circumference of the Earthdivided by m in longitude and divided by n-m in latitude

Page 6: Gravity Summary

http://en.wikipedia.org/wiki/Image:Harmoniques_spheriques_positif_negatif.png

Page 7: Gravity Summary

Gravity SummaryThe coefficients are computed as:

V=(GM/r) n=0∞ m=0

n (R/r)n (Cnm cos m + Snm sin m) Pnm (sin )

the Stokes’ Coefficient up to n=2 have a clear physical meaning

n=0: C=1 and S=0 so the first term of the spherical harmonics is only

V= GM/r

That is the gravity field of a point mass!

Page 8: Gravity Summary

Gravity Summary

V=(GM/r) n=0∞ m=0

n (R/r)n (Cnm cos m + Snm sin m) Pnm (sin )

For

n=1: C10 = zCM C11 = xCM S11 = yCM

The Stokes coefficient are the coordinates of the Center of Mass.

If the Center of Mass is the origin of our system they are zero!

Page 9: Gravity Summary

Gravity Summary

V=(GM/r) n=0∞ m=0

n (R/r)n (Cnm cos m + Snm sin m) Pnm (sin )

For

n=2: C20 = -1/(MR2) (I33- 0.5(I22+I11)) Difference diagonal term of inertia tensor

C21 = I13/(MR2) S21 = I23/(MR2)

C22 = (I22-I11)/(4MR2) S22 = I12/(2MR2)

The max inertia axys is very close to the rotation axis z so I13 and I23 are small

The other term are giving us the flattened shape of the Earth.

Essentially the degree 2 of the spherical armonics are giving the correction to the potential due to the elliptical shape.

Page 10: Gravity Summary

Often the potential is also written as a taylor expansion of the term r

V = −GM

r+GMR2

2r3J2 3sin

2 φ −1( )

J2MR2 =C − A

C = x 2 + y 2( )dm∫A = y 2 + z2( )dm∫

J is derived by precession of rotational axis or satellite orbits

Page 11: Gravity Summary

Moment inertia homogeneous sphere:2/5 MR2 ~ 0.4 MR2

For Earth ~0.3307 MR2

For Moon ~0.3935 MR2

Page 12: Gravity Summary

Moment inertia homogeneous sphere:2/5 MR2 ~ 0.4 MR2

For Earth ~0.3307 MR2

For Moon ~0.3935 MR2

The Earth has more mass close to the center

The moon is almost homogeneous (max radius metallic core 300km)

g =∇V ⇒∝1

r2

Mars: 0.366; Venus 0.33

Page 13: Gravity Summary

Gravity Summary

In first approximation we can chose for the shape of the Earth an ellipsoid of rotation defined essentially by the degree n=2 m=0 of the potential field plus the centrifugal potential. This is known as ellipsoid of reference.

In general all the measure of gravity acceleration and geoid are referenced to this surface. The gravity acceleration change with the latitutde essentially for 2 reasons: the distance from the rotation axis and the flattening of the planet.

The reference gravity is in general expressed by

g() = ge (1 + sin2 +sin4 )

and are experimental constants

= 5.27 10-3 =2.34 10-5 ge=9.78 m s-2

From Fowler

Page 14: Gravity Summary

Gravity Summary

A better approximation of

the shape of the Earth is

given by the GEOID.

The GEOID is an

equipotential surface

corresponding to the

average sea level surface

From Fowler

Page 15: Gravity Summary

H elevation over Geoidh elevation over ellipsoid

N=h-HLocal Geoid anomaly

Page 16: Gravity Summary

Geoid Anomaly

gΔh=-ΔV

Page 17: Gravity Summary

Geoid Anomaly

gΔh=-ΔV

Dynamic Geoid

Page 18: Gravity Summary

Geoid Anomaly

Page 19: Gravity Summary