2025-02-23T13:17:11-05:00 DEBUG: VuFindSearch\Backend\Solr\Connector: Query fl=%2A&wt=json&json.nl=arrarr&q=id%3A%22irk-123456789-95454%22&qt=morelikethis&rows=5
2025-02-23T13:17:11-05:00 DEBUG: VuFindSearch\Backend\Solr\Connector: => GET http://localhost:8983/solr/biblio/select?fl=%2A&wt=json&json.nl=arrarr&q=id%3A%22irk-123456789-95454%22&qt=morelikethis&rows=5
2025-02-23T13:17:11-05:00 DEBUG: VuFindSearch\Backend\Solr\Connector: <= 200 OK
2025-02-23T13:17:11-05:00 DEBUG: Deserialized SOLR response
Оптимизация перелетов космического аппарата между отдаленными эллиптическими орбитами
A problem of optimization of trajectories, control and parameters of the spacecraft engine system of microthruster of constant power with energy storage is solved. The spacecraft is done the orbit adjust maneuver of synchronous essential change the major semi-axis, excentricity and angle of slope...
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| Main Authors: | , |
|---|---|
| Format: | Article |
| Language: | Russian |
| Published: |
Інститут механіки ім. С.П. Тимошенка НАН України
2010
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| Series: | Прикладная механика |
| Online Access: | http://dspace.nbuv.gov.ua/handle/123456789/95454 |
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