Zobrazeno 1 - 10
of 39
pro vyhledávání: '"Ivan I. Kosenko"'
Publikováno v:
INTERNATIONAL CONFERENCE OF COMPUTATIONAL METHODS IN SCIENCES AND ENGINEERING ICCMSE 2020.
An attitude dynamics of a satellite with a variable properties of inertia under the central of gravity is analyzed. One assumes that the satellite is equipped by rotors with a variable kinetic moments. We suppose that the satellite mass center moves
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a80cea733fd1008e8ec6f2dc3fa4901d
https://doi.org/10.1063/5.0048016
https://doi.org/10.1063/5.0048016
Publikováno v:
Multibody System Dynamics. 45:273-292
An omni-wheel is defined as a wheel having rollers along its rim. Vehicles with omni-wheels are able to maneuver in any direction. For modeling the dynamics of omni-wheels we use general formalisms, previously developed by the authors for the multibo
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::ce70ddb05575e160ddc6a2de13dfc023
https://doi.org/10.1007/s11044-018-09649-x
https://doi.org/10.1007/s11044-018-09649-x
Publikováno v:
Acta Astronautica. 143:126-132
Relative equilibria of a pendulum attached to the surface of a uniformly rotating celestial body are considered. The locations of the tether anchor that correspond to a given spacecraft position are defined. The domains, where the spacecraft can be h
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::0d69eb11d1a4fc0be22ebdf0b6c8e74d
https://doi.org/10.1016/j.actaastro.2017.11.018
https://doi.org/10.1016/j.actaastro.2017.11.018
Publikováno v:
IFAC-PapersOnLine. 51:867-872
Motion of a pendulum tethered via a tether to a rotating asteroid of arbitrary shape is considered. Equations of motion are obtained, conditions for the tether to be stretched are investigated. The constraint releasing processes, as well as constrain
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::70b00f9b0a6ec1df767639779c7e1e15
https://doi.org/10.1016/j.ifacol.2018.04.023
https://doi.org/10.1016/j.ifacol.2018.04.023
Publikováno v:
Doklady Physics. 62:359-362
The motion of a massive point (a bead) over the surface of a uniformly rotating asteroid is considered. It is assumed that the force of dry friction acts between the point and the asteroid surface. The sets of nonisolated positions of relative equili
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::bd2a8f4641192cda1130bdeb847d81dc
https://doi.org/10.1134/s1028335817070084
https://doi.org/10.1134/s1028335817070084
Publikováno v:
Multibody Dynamics 2019 ISBN: 9783030231316
We consider the motion of a vehicle with omni-wheels that moves along a horizontal plane without slipping. The mass of the rollers is non-zero and influences the dynamics of the system. The system is a multibody system of rigid bodies with non-holono
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::dd086b57a75435228a38842baeacec9a
https://doi.org/10.1007/978-3-030-23132-3_62
https://doi.org/10.1007/978-3-030-23132-3_62
Publikováno v:
Multibody Dynamics 2019 ISBN: 9783030231316
Our goal is to build up an efficient computer model of the omni-vehicle comprising several omni-wheels (each one carries several freely rotating rollers on its periphery); the vehicle rolls without control on a horizontal plane. For simulating contac
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::cfca266733dbbb24394f660ec30cffce
https://doi.org/10.1007/978-3-030-23132-3_61
https://doi.org/10.1007/978-3-030-23132-3_61
Publikováno v:
Celestial Mechanics and Dynamical Astronomy. 131
The dynamics of a spacecraft with variable mass distribution is considered, assuming a central Newtonian gravitational field. The equations of spatial attitude motion are derived within the framework of the so-called satellite approximation and exami
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::03dfd94f204867cfa0a2b0d9a8f3e2c9
https://doi.org/10.1007/s10569-018-9874-0
https://doi.org/10.1007/s10569-018-9874-0
Autor:
Alexander A. Burov, Ivan I. Kosenko
Publikováno v:
AIP Conference Proceedings.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::245076855cefb01fa766935c7aaedb6a
https://doi.org/10.1063/1.5034610
https://doi.org/10.1063/1.5034610
Publikováno v:
Acta Astronautica. 116:349-354
We consider the problem of in-plane rotations of a space elevator with variable tether length attached to a surface of one of the primaries in a double system. The planet and its moon (or two asteroids) move about their center of mass in unperturbed
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::4d36f56faaee14525019ca27111efe95
https://doi.org/10.1016/j.actaastro.2015.05.018
https://doi.org/10.1016/j.actaastro.2015.05.018