??????????? ??????????? ????????????? ????????? ???????? ? ?????? ??????? ??????????? ?????????? ????????
Електронний архів Житомирського державного технологічного університету
View Archive Info| Field | Value | |
| Title |
??????????? ??????????? ????????????? ????????? ???????? ? ?????? ??????? ??????????? ?????????? ????????
Organization of optimum near-earth space maneuver in densely populated conditions of outer space |
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| Creator |
??????????, ?.?.
Kanevskyy, L.B. |
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| Subject |
????????????? ???????
??????????? ??? ????????? ???????? ?????? ?????????? ??????? ?????????? ???????? ??????????? ???????????? ????????? near-Earth space orbital motion space objects maneuver spacecraft optimal transitions probability of a dangerous convergence |
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| Description |
???????????? ???????, ?? ????????????? ? ??????, ?????????? ???????? ?????????? ?????????? ??? ????????? ????????? ????????, ?? ???????????? ? ???????????? ?? ????????????? ???????, ?? ???? ????????? ????????? ???????? ? ?????? ???????, ?? ?????? ??????????. ???? ??????? ???????????? ??????? ???????? ????????? ???????? ??????? ?????? ????? ?? ?????????? ??????? ???????????? ? ?????????? ????????. ? ?????? ???? ?????????????? ??????? ?????????? ??? ????? ???? ?????????? ??????? ??? ???????? ? ?????? ?????? ?? ???? ? ?????? ????? ? ???????????? ????????????? ?????????. ????????????? ??????? ???? ??????????? ????????? ???????? ??????? ????? ? ??????????? ??????? ??????????? ?????????? ????????. ??? ????? ???????? ?????? ??????? ?? ?? ?????? ?????????????? ?????, ? ?? ??????????? ??????????? ???????????? ?????????, ?? ??????? ????? ?????????? ??????????? ???????????? ????? ?? ???????? ????????? ???? ?????????? ???????????? ?????? ?????????? ???????????? ????????? ??? ?????????? ????????? ? ?????????????? ????????. ?????????? ??????????? ??????????? ?????????? ???????? ?????????? ??????? ??? ????????????? ???????? ???? ???? ??????????? ? ??? ??????????????? ?????????? ????? ?? ????? ?????????? ???????? ?? ??? ??? ????????? ?????. Relevance of the issues addressed in the article, due to the rapid growth of the imbalance between the number of spacecraft launched and operate in Earth orbit, and with a number of spacecraft and launch units that are derived therefrom. The need to ensure the safety of spacecraft requires a search for new and effective methods of maneuvering in space. The paper analyzed the system of indicators to change the motion of the spacecraft during the transition from one orbit to another in the set point with minimal costs. An approach for the organization of space maneuvers around the Earth with the densely populated space, parameter optimization methodology disclosed transition active spacecraft from orbit to orbit. At the same time the emphasis was not on the specific characteristics of the orbits, and to optimize the pulse of the orbital flight, and the basic principles for improving the problem of determining the probability of dangerous rapprochement between space objects in near-Earth space. The methodology of optimizing the parameters of the spacecraft transition between coplanar orbits, can be used for placing nekomplanarnoho orbits provided the amendments to the angle between the planes of the orbits. |
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| Date |
2016-03-18T07:39:56Z
2016-03-18T07:39:56Z 2015 |
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| Type |
Article
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| Identifier |
http://eztuir.ztu.edu.ua/123456789/2074
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| Language |
uk
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| Relation |
?????? ????. ?????: ???????? ?????;2(73)
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| Publisher |
????
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