Physics
Scientist
A Spacecraft Control Scheme for the Outbound Leg of the Artificial Earth Satellite Flight
An analytical method for determining the elements of Keplerian orbits according to two positions of the spacecraft
An approximate analytical method for calculating the trajectories of a flight vehicle in the atmosphere
Analytical method for determining Keplerian orbital elements from two spacecraft positions.
Applying the theory of Markovian processes to the motion of spacecraft in the atmosphere.
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