Contribution of earth oblateness to gravity torque on a satellite.
Earth oblateness effect on torque experienced in nonuniform geogravitational field by satellite with unequal principal moments of inertia
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Earth oblateness effect on torque experienced in nonuniform geogravitational field by satellite with unequal principal moments of inertia
Solar oblateness and Mercury perihelion advance, showing turbulent viscosity forces acting on photospheric meridional currents as possible distortion cause
Lunar orbit precession due to quadrupole moment of sun arising from solar oblateness
Pendulum simulation of liquid propellant sloshing in spherical and oblate spheroidal tanks
Free vibrations of thin isotropic oblate spheroidal shells
Analytical method for determining axisymmetric longitudinal mode shapes and frequencies of incompressible and inviscid fluid in pressurized flexible oblate spheroidal propellant tank
Time history of satellite around oblate planet
Orbital regression of synchronous satellites due to combined gravitational effects of sun, moon, and oblate earth
Satellite motion for all inclinations around oblate planet with potential including second and fourth zonal harmonics
Planetary gravitation and oblateness used for parking orbit alignment in Mars mission
Satellite orbit secular perturbations resulting from central body oblateness for 2m-th zonal harmonics and gravitational attraction of third body
Liquid sloshing under moderately low simulated gravity in oblate ellipsoidal tank geometries
Idealized point mass motion in axisymmetric gravitational field, discussing orbital stability about oblate planet
Gravitational and magnetic torque effect on rotational motion of triaxial rigid body in regressing orbit about oblate primary mass
Drag coefficients of oblate spheroid and sphere at Mach numbers from 1.70 to 10.49
Relative motion analysis for two satellites of oblate planet
Earth oblateness effects on lunar and interplanetary trajectories, using algorithm based on orbital elements variations
Procedures for determining launch window for SERT 2 mission and effect of low thrust and earth oblateness orbit perturbations