Construction of optimum controls and trajectories of motion of the center of masses of a spacecraft equipped with the solar sail and low-thrust engine, using quaternions and Kustaanheimo-Stiefel variables
Crossref DOI link: https://doi.org/10.1134/S0010952514060057
Published Online: 2014-12-21
Published Print: 2014-11
Update policy: https://doi.org/10.1007/springer_crossmark_policy
Sapunkov, Ya. G.
Chelnokov, Yu. N.
Text and Data Mining valid from 2014-11-01