Physics – Geophysics
Multistep algorithms for the correction of the orbit of an earth satellite by a low-thrust engine
Optimal acceleration of a spacecraft with an electroreactive engine in the case of constrained velocity of rotation of the thrust vector
Optimal acceleration of spacecraft with electroreactive engine for bounded rate of rotation of thrust vector
Optimal control of the elliptical orbit of an earth satellite with a low-thrust engine
Potential and Limitations of the Archaeo-Geophysical Techniques
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