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Chapter 5 Perturbation Models <strong>of</strong> IGSO,GEO and MEO <strong>Satellite</strong>s <strong>Orbit</strong>s<br />

CHAPTER 5 PERTURBATION MODELS OF IGSO, GEO and MEO<br />

SATELLITE ORBITS<br />

The performances <strong>of</strong> IGSO, GEO and MEO satellite orbits will be affected by many perturbations such as the<br />

non-central part <strong>of</strong> the Earths gravitational potential, gravitational effects <strong>of</strong> Sun and Moon, solid earth tidal<br />

effects, solar radiation pressure, Albedo radiation pressure, gravitational effects <strong>of</strong> ocean tides, gravitational<br />

effects <strong>of</strong> the planets, relativistic corrections, thermal emission <strong>of</strong> the satellite etc. Because IGSO, GEO and<br />

MEO satellite orbits are far away from the earth, the effects <strong>of</strong> earth tides, ocean tides and earth radiation are<br />

much smaller. Hence the non-central part <strong>of</strong> the Earth, the gravitational effects <strong>of</strong> Sun and Moon and solar<br />

radiation pressure play a major role in the perturbations on IGSO, GEO and MEO satellite orbits. In this chapter,<br />

the computations <strong>of</strong> these three perturbation models will be discussed. The major literatures on this topic are<br />

referred to Soop (1994), Tscherning (1976, 1977).<br />

5.1 The Earth Gravitational Perturbation<br />

The earth geopotential is represented as a point mass and an expansion <strong>of</strong> spherical harmonics to represent the<br />

nonspherical effect <strong>of</strong> the Earth mass. The geopotential can be expressed by (Rothacher, 1992)<br />

GM<br />

U =<br />

r<br />

+ GM<br />

N<br />

n<br />

��<br />

n=<br />

2 m=<br />

0<br />

r<br />

n<br />

e<br />

n+<br />

1<br />

a<br />

P<br />

nm<br />

(sin ϕ )( C cos mλ<br />

+ S sin mλ)<br />

(5-1)<br />

where<br />

G Newtonian Gravitational Constant<br />

M the Earth’s mass (GM=398.600415×10 12 m 3 s -2 )<br />

Pnm (sin ϕ)<br />

associated Legendre function<br />

λ, ϕ<br />

geographic longitude and latitude <strong>of</strong> satellite<br />

spherical harmonic coefficients.<br />

Cnm , Snm<br />

nm<br />

nm<br />

In the equation above, the first term is the point mass part. The other terms are an expansion <strong>of</strong> spherical<br />

harmonics to represent the nonspherical effects <strong>of</strong> the earth mass, i.e. the Earth gravitational perturbation.<br />

The forces produced by the geopotential are computed by<br />

N<br />

��<br />

n=<br />

2 m=<br />

0<br />

43<br />

n<br />

ae<br />

n+<br />

m+<br />

1<br />

∂U<br />

∂U<br />

∂U<br />

GM<br />

( m)<br />

grad(<br />

U ) = ( , , ) = grad(<br />

) + GM grad{<br />

Pn<br />

(sin ϕ)(<br />

Cnmξ<br />

m + S nmηm<br />

)}<br />

∂x<br />

∂y<br />

∂z<br />

r<br />

r<br />

n<br />

5.1.1 Computation <strong>of</strong> Legendre Polynomials<br />

From Eq.(5-1) it can be seen that in order to compute the geopotential, the first step is computation <strong>of</strong> the<br />

Legendre polynomials.<br />

The Legendre polynomials Pn as a function <strong>of</strong> the independent variable x can be defined by:<br />

n<br />

1 d 2 n<br />

P n ( x)<br />

= ( x − 1)<br />

(5-3)<br />

n n<br />

2 n!<br />

dx<br />

For a given value <strong>of</strong> x, the Legendre polynomials Eq.(5-3) can be calculated by the following recursive formula<br />

with starting values:<br />

P ( x)<br />

= 1;<br />

P ( x)<br />

= x<br />

0<br />

2n<br />

−1<br />

pn<br />

( x)<br />

= xP<br />

n<br />

1<br />

n−1<br />

n −1<br />

( x)<br />

− P<br />

n<br />

n−2<br />

( x)<br />

if n ≥ 2<br />

(5-2)<br />

(5-4)

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