Multi-structural estimation of an integrated navigation system of a reusable spacecraft |
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Authors: | V A Pogorelov |
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Institution: | (1) Rostov Military Institute of Missile Corps, Rostov-on-Don, 344027, Russia |
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Abstract: | An approach to the synthesis of an integrated navigation system is considered for a reusable space-craft that performs an arbitrary spatial maneuver under the conditions of internal and external disturbances. The offered approach provides for a noise-suppressing solution of the navigation problem, both in a regular mode of spacecraft motion, and during its descent along the unplanned trajectory. |
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Keywords: | PACS" target="_blank">PACS 95 10 Eg |
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