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
Sapunkov, Ya. G., Chelnokov, Yu. N.Volume:
52
Language:
english
Journal:
Cosmic Research
DOI:
10.1134/S0010952514060057
Date:
November, 2014
File:
PDF, 437 KB
english, 2014