Accuracy Analysis of Lunar Lander Terminal Guidance Algorithm
<p>This article studies a proposed analytical algorithm of the terminal guidance for the lunar lander. The analytical solution, which forms the basis of the algorithm, was obtained for a constant acceleration trajectory and thrust vector orientation programs that are essentially linear with ti...
| Main Authors: | , |
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| Format: | Article |
| Language: | Russian |
| Published: |
MGTU im. N.È. Baumana
2017-01-01
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| Series: | Nauka i Obrazovanie |
| Subjects: | |
| Online Access: | http://technomag.edu.ru/jour/article/view/957 |