Pulsed Optimal Spacecraft Orbit Reorientation by Means of...

Pulsed Optimal Spacecraft Orbit Reorientation by Means of Reactive Thrust Orthogonal to the Osculating Orbit. I

Sapunkov, Ya. G., Chelnokov, Yu. N.
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Volume:
53
Language:
english
Journal:
Mechanics of Solids
DOI:
10.3103/S0025654418080083
Date:
September, 2018
File:
PDF, 415 KB
english, 2018
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