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Satellite Orbit and Ephemeris Determination using Inter Satellite Links

Satellite Orbit and Ephemeris Determination using Inter Satellite Links

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<strong>Inter</strong> <strong>Satellite</strong> <strong>Links</strong><strong>Orbit</strong> ComputationU Gravity potentialGM Earth's gravity constantr magnitude of radius vector (of an arbitrary point)a Earth's equatorial radiusn,m Degree <strong>and</strong> order of spherical harmonicsP nm Legendre functionsC nm ,S nm Coefficients of spherical harmonicsϕ Latitudeλ LongitudeThe Legendre polynomials P n <strong>and</strong> associated functions P nm are defined as<strong>and</strong>Pn1 d 2 nn (x) = (x −1)n n2 n! dxEq. 4.2-12Pnm(x) = (1 − x2 m / 2)dmPnmdx(x)Eq. 4.2-13The force acting on a point in the gravitation field is obtained by computing the gradient ofthe potential. Eq. 4.2-14∂U∂U∂Ug = grad(U) = ( , , )∂x∂y∂zThis analytical expression is not very well suited for implementation. Soop (1994) indicates arecursive method for computing the Legendre polynomials <strong>and</strong> functions, as well as thepartial derivatives required to compute the gravity force.4.2.1.1 Computation of Legendre Polynomials <strong>and</strong> FunctionsThe Legendre polynomials can be computed recursively <strong>using</strong> starting values for the first twoterms:P (x) = 1;0P (x) = x2n −1pn(x) = ⋅ xPnn1−1n −1(x) − ⋅ Pnn−2(x) if n ≥ 2Eq. 4.2-15The associated Legendre functions are obtained in two steps. First, the m-fold derivative ofeach polynomial P n (x) is computedmPnm(m) d (x)P n (x) =dxEq. 4.2-16R. Wolf Page 27

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