Physics
Scientist
Analysis of optimum transfer with 180 deg angular distance between coplanar elliptic orbits
Investigation of an optimal orbital transfer with an angular range of 180 deg between coplanar elliptical orbits
On a method for the autonomous refinement of the motion parameters of a orbital spacecraft
Refinement of the motion parameters of an orbital spacecraft by means of navigation satellites
Study of optimal multimomentum transfers with bounded time between close near-circular orbits
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