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Correction of spacecraft trajectory during its transition into circular satellite orbit using atmospheric braking with uncertain atmospheric parameters
| Authors: Kazakovtsev V.P. , Koryanov V.V. , Zaw Min Tun | Published: 06.10.2015 |
| Published in issue: #5(104)/2015 | |
| DOI: | |
| Category: Aviation and Rocket-Space Engineering | Chapter: Aircraft Dynamics, Ballistics, Motion Control | |
| Keywords: orbit, spatial motion, spacecraft, braking in atmosphere, heat flow, dynamic pressure | |