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Spacecraft optimal control in drag braking flight segment during insertion into orbit of Mars artificial satellite
| Authors: Sokolov N.L. | Published: 21.12.2015 |
| Published in issue: #6(105)/2015 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: spacecraft, insertion into orbit, combined insertion profile, optimal control, research technique, analytical algorithm, implementation efficiency | |