4.1.2                 Gravity model formulation

Without compromising the general validity of underlying theories, all subsequent gravity model discussions are focused on the Earth. The gravity acceleration acting on a point mass, which is external to the central body, is the gradient of the potential function U of that body. The corresponding geopotential surface satisfies the so called Laplace equation:

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The corresponding perturbing acceleration can be determined from equation (4‑3) by means of computationally efficient recursion algorithms (e.g. as in [RD.1]).

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where

 is the 2nd time derivative of the position vector.

The solution U of the partial differential equation (4‑2) is typically written in the form of a series expansion, in terms of so-called surface spherical harmonic functions, for a location defined in spherical coordinates r, λ, ϕ.

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where

GM = μ             is the gravity constant of the Earth (M being its mass);

μ = 3,98604415×1014 m3s-2 for the EIGEN-GL04C model

ae        is the mean equatorial radius of the Earth;

ae = 6 378 136,460 m for the EIGEN-GL04C model

r         is the radial distance from centre of the Earth to satellite

N       is the maximum degree of the expansion

l         is the degree of a certain harmonic function

m        is the order of a certain harmonic function

Clm, Slm              are coefficients that determine amplitude and phase of a certain harmonic function

λ        is the geodetic longitude of the sub-satellite point

ϕ        is the geodetic latitude of the sub-satellite point

Plm     are associated Legendre functions of the first kind, of degree l and order m; recurrance relations for these functions are available in the literature (e.g. [RD.1]).

 

A gravity model consists of adopted values for GM, ae, and a set of model coefficients Clm, Slm. Practical implementations of gravity models, e.g. for numerical integration of a satellite orbit, are typically interested in the gravity acceleration resulting from the potential function U in (4‑4). Corresponding partial derivatives of (4‑4) in Cartesian coordinates of an Earth-fixed system x, y, z can be computed recursively (see [RD.1]).

The model coefficients Clm, Slm are typically provided in their normalized versions, according to (4‑5) in order to limit their numerical range for higher degrees and orders.

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The Legendre functions Plm (sin ϕ) in this case are normalized by the inverse of the square root in equation (4‑5).