Attitude control algorithms for a descent vehicle returning from the moon
We consider the problem of attitude control of a descent vehicle in the Earth’s atmosphere returning from the Moon. A stabilization algorithm with a deadband and the optimal parameters, obtained with the numerical method, provide adequate landing accuracy and an allowable load factor under the influ...
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| Veröffentlicht in: | Journal of computer & systems sciences international 2017-05, Vol.56 (3), p.483-491 |
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| container_end_page | 491 |
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| container_issue | 3 |
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| container_title | Journal of computer & systems sciences international |
| container_volume | 56 |
| creator | Evdokimov, S. N. Klimanov, S. I. Korchagin, A. N. Mikrin, E. A. Sikharulidze, Yu. G. Tuchin, A. G. |
| description | We consider the problem of attitude control of a descent vehicle in the Earth’s atmosphere returning from the Moon. A stabilization algorithm with a deadband and the optimal parameters, obtained with the numerical method, provide adequate landing accuracy and an allowable load factor under the influence of a set of disturbances. Using the method of mathematical simulation, it is shown that the fuel consumption is reduced by ~30% in comparison with the initial stabilization parameters for the descent from a near-Earth orbit. |
| doi_str_mv | 10.1134/S1064230717030091 |
| format | Article |
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N. ; Klimanov, S. I. ; Korchagin, A. N. ; Mikrin, E. A. ; Sikharulidze, Yu. G. ; Tuchin, A. G.</creator><creatorcontrib>Evdokimov, S. N. ; Klimanov, S. I. ; Korchagin, A. N. ; Mikrin, E. A. ; Sikharulidze, Yu. G. ; Tuchin, A. G.</creatorcontrib><description>We consider the problem of attitude control of a descent vehicle in the Earth’s atmosphere returning from the Moon. A stabilization algorithm with a deadband and the optimal parameters, obtained with the numerical method, provide adequate landing accuracy and an allowable load factor under the influence of a set of disturbances. Using the method of mathematical simulation, it is shown that the fuel consumption is reduced by ~30% in comparison with the initial stabilization parameters for the descent from a near-Earth orbit.</description><identifier>ISSN: 1064-2307</identifier><identifier>EISSN: 1555-6530</identifier><identifier>DOI: 10.1134/S1064230717030091</identifier><language>eng</language><publisher>Moscow: Pleiades Publishing</publisher><subject>Accuracy ; Computer simulation ; Control ; Control algorithms ; Control Systems of Moving Objects ; Descent ; Energy efficiency ; Engineering ; Fuel consumption ; Fuels ; Mechatronics ; Numerical analysis ; Orbital stability ; Robotics ; Spacecraft ; Spacecraft attitude control ; Stabilization ; Studies</subject><ispartof>Journal of computer & systems sciences international, 2017-05, Vol.56 (3), p.483-491</ispartof><rights>Pleiades Publishing, Ltd. 2017</rights><rights>Journal of Computer and Systems Sciences International is a copyright of Springer, 2017.</rights><lds50>peer_reviewed</lds50><woscitedreferencessubscribed>false</woscitedreferencessubscribed><citedby>FETCH-LOGICAL-c316t-30d6ef9ca865e9df2d8854daff8204a50c548f0138347665b241b926e40656753</citedby><cites>FETCH-LOGICAL-c316t-30d6ef9ca865e9df2d8854daff8204a50c548f0138347665b241b926e40656753</cites></display><links><openurl>$$Topenurl_article</openurl><openurlfulltext>$$Topenurlfull_article</openurlfulltext><thumbnail>$$Tsyndetics_thumb_exl</thumbnail><linktopdf>$$Uhttps://link.springer.com/content/pdf/10.1134/S1064230717030091$$EPDF$$P50$$Gspringer$$H</linktopdf><linktohtml>$$Uhttps://link.springer.com/10.1134/S1064230717030091$$EHTML$$P50$$Gspringer$$H</linktohtml><link.rule.ids>314,780,784,27924,27925,41488,42557,51319</link.rule.ids></links><search><creatorcontrib>Evdokimov, S. 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| subjects | Accuracy Computer simulation Control Control algorithms Control Systems of Moving Objects Descent Energy efficiency Engineering Fuel consumption Fuels Mechatronics Numerical analysis Orbital stability Robotics Spacecraft Spacecraft attitude control Stabilization Studies |
| title | Attitude control algorithms for a descent vehicle returning from the moon |
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