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Journal description
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Details for article 13 of 14 found articles
| Title: |
The use of solutions to problems of spacecraft trajectory optimization in impulse formulation when solving the problems of optimal control of trajectories of a spacecraft with limited thrust engine: I |
| Author: |
Grigoriev, I. S. Grigoriev, K. G. |
| Appeared in: |
Cosmic research |
| Paging: | Volume 45 (2007) nr. 4 pages 339-347 |
| Year: |
2007 |
| Contents: | |
| Publisher: |
Nauka/Interperiodica, Moscow |
| Source file: |
Elektronische Wetenschappelijke Tijdschriften |
Details for article 13 of 14 found articles
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