Lunar communications with libration-point satellites.
Satellite motion in libration point vicinity, neglecting lunar eccentricity and solar perturbation, discussing lunar communication system utilizing libration point satellites
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Satellite motion in libration point vicinity, neglecting lunar eccentricity and solar perturbation, discussing lunar communication system utilizing libration point satellites
Three body stellar problem libration calculation using nonlinear mechanics methods, and application to lunar satellite perturbation by earth and lunar gravitational effects
Interplanetary magnetic field perturbations by lunar wake using plasma flow model
Three-dimensional guidance scheme for decending from lunar orbit to hovering position based on linear theory of perturbations
Harmonic analysis method used to derive formulae for long periodic perturbations of lunar satellites
Determining higher order perturbations for lunar orbiter by Krylov-Bololiubov and Poincare methods
Interplanetary magnetic field measurements in lunar wake, noting magnetic perturbations pattern and absence of shocks
Lunar-solar perturbation effect on satellites with eccentric orbits, noting lifetimes on perigee heights
Perturbations of the solar wind downstream of the moon and lying outside of the rarefaction wave that defines the diamagnetic cavity are used to define possible source regions comprised of intrinsically magnetized areas of the moon. A map of the moon is constructed showing that a model in which the sources are exposed to the grazing solar wind during the lunation yields a selenographically invariant set of regions strongly favoring the lunar highlands over the maria. An alternative model with the source due to electromagnetic induction is explored. The ages of the field sources should be consistent with those based on the basalt ages and possibly far older if the sources are connected with the formation of the highland rocks themselves. The perturbations are tentatively identified as weak shock waves, and a Mach angle in accord with nominal values for the solar wind is found.
Explorer 33 and Explorer 35 measurements of perturbed interplanetary magnetic field in lunar wake
Lunar ephemeris for nanosecond resolution laser ranging systems by literal and numerical integration techniques
The orbital decay of the International Sun-Earth Explorer (ISEE-1) and ISEE-2 spacecraft was studied. The perturbative forces due to the nonspherical components of the earth's gravitational field, atmospheric drag, solar radiation pressure, and third-body perturbations are examined. The dynamics of the earth-spacecraft-moon system is analyzed as well. Various scenarios using the perturbative forces in conjunction with propulsive energy are evaluated to determine the requirements for extending the lifetime of this type of mission.
Classification of lunar satellite orbits perturbed by earth and by nonsphericity of lunar gravitational field
Computer derived orbital parameter variations for forty hour period after insertion into two reference Apollo lunar parking orbits
Harmonic models and Doppler data used to analyze orbital perturbation of Lunar Orbiter
Effects of solar and lunar tides on motion of artificial earth satellite
Lunar and solar effects on motion of close earth satellites
Lunar solar perturbation effect on orbital lifetimes of artificial satellites with highly eccentric orbits