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EQUATIONS OF MOTION
THE CASE OF SMALL ECCENTRICITY
THE GENERAL SCHEME OF THE FURTHER APPROXIMATIONS
1 other sections not shown
8-1858 National Aeronastics a0 sin2 Aeronastics and Npace andk2 Apteemer argument of perigee Artificial Satellite CLONE EARTH NATELLITEN CLOSE EARTH SATELLITES close satellites corresponds cos2 cos4 oj cosh2 CRITICAL INCLINATION elliptic integrals Equation 28 equations of motion functions and elliptic Hamiltonian higher order terms higher order theory inclination is developed INCLINATION OF CLONE integration of Equation intermediary solutions Izsak Jacob5an elliptic func Jacobian elliptic functions Jacobian zeta-function k5nd are necessary kind are required libration moderate eccentricity motion of close NANA 18 NANA TECHNICAL NOTE NASA NANA TN Npace Administration numerical integration obtain further approximations order of j2 order of magni order of magnitude OTN price periodic function plane sym power series Q sin4 second kind second order shown that solutions sin&jj sin2 oj small eccentricity sn2 A.u TECHNICAL NOTE 8-1858 THEORY OF CRITICAL third k5nd third order tude are included vicinity zeta-function are required zonal harmonics