Отрывок: 4. Research method of attitude motion of variable mass coaxial bodies and unbalanced gyrostat Let's refer to a motion of coaxial bodies (unbalanced gyrostat) of variable mass under an action of dissipative and boosting external moments depending on components of angular velocities. Let the gyrostat consists of dynamically symmetrical main body (coaxial body 2) of a constant mass and a rotor (coaxial body 1) of the variable mass, which remain...
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dc.contributor.authorBalakin V. L.ru
dc.contributor.authorDoroshin A. V.ru
dc.contributor.authorThe Ministry of Education and Science of the Russian Federationru
dc.contributor.authorSamara State Aerospace University (National Research University)ru
dc.contributor.authorFlight dynamics and control systems departmentru
dc.coverage.spatialКА с двойным вращениемru
dc.coverage.spatialдинамические системыru
dc.coverage.spatialгироскопическая системаru
dc.coverage.spatialгиростатыru
dc.coverage.spatialпеременная структураru
dc.coverage.spatialматематическое моделированиеru
dc.coverage.spatialстранный аттракторru
dc.coverage.spatialкосмические аппаратыru
dc.coverage.spatialхаотические режимы движенияru
dc.coverage.spatialхаос769221ru
dc.coverage.spatialпространственное движениеru
dc.coverage.spatialспутники-гиростатыru
dc.coverage.spatialрегулярные режимы движенияru
dc.creatorBalakin V. L., Doroshin A. V.ru
dc.date.issued2012ru
dc.identifierRU/НТБ СГАУ/WALL/629.78/B 18-630470ru
dc.identifier.citationBalakin, V. L. Attitude Dynamics and Control of a Dual-Spin-Spacecraft, Gyrostat-Satellites and Nanosatellites with Multyrotor Systems [Электронный ресурс] : Electronic Textbook / V. L. Balakin, A. V. Doroshin ; The Ministry of Education and Science of the Russian Federation, Samara State Aerospace University (National Research University), Flight dynamics and control systems d. - Samara, 2012. - on-lineru
dc.description.abstractТруды сотрудников СГАУ(электрон. версия).ru
dc.description.abstractИспользуемые программы: Adobe Acrobat.ru
dc.format.extentElectronic text and graphic data (1 файл : 2,17 Mb)ru
dc.language.isorusru
dc.relation.isformatofAttitude Dynamics and Control of a Dual-Spin-Spacecraft, Gyrostat-Satellites and Nanosatellites with Multyrotor Systems [Электронный ресурс] : Electroru
dc.titleAttitude Dynamics and Control of a Dual-Spin-Spacecraft, Gyrostat-Satellites and Nanosatellites with Multyrotor Systemsru
dc.typeTextru
dc.subject.rugasnti55.49ru
dc.subject.udc629.78(075)ru
dc.textpart4. Research method of attitude motion of variable mass coaxial bodies and unbalanced gyrostat Let's refer to a motion of coaxial bodies (unbalanced gyrostat) of variable mass under an action of dissipative and boosting external moments depending on components of angular velocities. Let the gyrostat consists of dynamically symmetrical main body (coaxial body 2) of a constant mass and a rotor (coaxial body 1) of the variable mass, which remain...-
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