Отрывок: The algorithms are based on the law of the Keplerian element changes. In [3] the law of the Keplerian element changes is following: 3 2 1 1 2 1 1( ) cos ( ) ( ) cos ( ) sin( ) dK f f dt ϑ λ ϑ λ λ= ⋅ + ⋅ ⋅ (6) The equation of motion (6) allows us to estimate locally optimal control laws for a solar sail spacecraft. The locally optimal control laws prov...
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dc.contributor.authorKhabibullin, R.M.-
dc.contributor.authorStarinova, O.L.-
dc.date.accessioned2018-05-18 10:52:37-
dc.date.available2018-05-18 10:52:37-
dc.date.issued2018-
dc.identifierDspace\SGAU\20180517\69427ru
dc.identifier.citationKhabibullin R.M. Mathematical modeling of the solar sail spacecraft three- dimensional motionin heliocentric coordinate system/R.M. Khabibullin, O.L. Starinova// Сборник трудов IV международной конференции и молодежной школы «Информационные технологии и нанотехнологии» (ИТНТ-2018) - Самара: Новая техника, 2018. - С.1706-1710ru
dc.identifier.urihttp://repo.ssau.ru/handle/Informacionnye-tehnologii-i-nanotehnologii/Mathematical-modeling-of-the-solar-sail-spacecraft-three-dimensional-motionin-heliocentric-coordinate-system-69427-
dc.description.abstractThe paper outlines the mathematical motion model of the solar sail spacecraft. The work considers the mathematical three-dimensional motion model of the perfect-reflection solar sail and the operational orbit maintenance and correction algorithms in heliocentric coordinate system. On the basis of the formulated mathematical model the special software complex for interplanetary transfer simulation is developed. Especially, the mission of the transfer of the spacecraft from the Earth’s orbit to the potentially hazardous asteroid is simulated. The obtained results during simulation demonstrate correctness and feasibility of the considered mathematical motion model.ru
dc.language.isoenru
dc.publisherНовая техникаru
dc.relation.ispartofseries3;228-
dc.subjectsolar sail spacecraftru
dc.subjectmathematical motion modelru
dc.subjectthree-dimensional motionru
dc.subjectheliocentric motionru
dc.titleMathematical modeling of the solar sail spacecraft three- dimensional motionin heliocentric coordinate systemru
dc.typeArticleru
dc.textpartThe algorithms are based on the law of the Keplerian element changes. In [3] the law of the Keplerian element changes is following: 3 2 1 1 2 1 1( ) cos ( ) ( ) cos ( ) sin( ) dK f f dt ϑ λ ϑ λ λ= ⋅ + ⋅ ⋅ (6) The equation of motion (6) allows us to estimate locally optimal control laws for a solar sail spacecraft. The locally optimal control laws prov...-
Располагается в коллекциях: Информационные технологии и нанотехнологии

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