Physics
Scientist
A condition for the boundedness of a spacecraft's orbit in the vicinity of a collinear libration center of the restricted elliptical three-body problem
Determination of the Trajectory of the Flight of a Space Craft when the Distribution Law of the Measurement Errors is Unknown
Evolution of Almost-Circular Artificial Earth Satellite Orbits under the Influence of Zonal Harmonics
Guaranteed Estimate of Precision in Determination of Spacecraft Motion
On the Possibility of Using the Gravitational Field of Jupiter to Fly at a given Distance from the Sun and to Escape from the Ecliptic Plane
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