Zobrazeno 1 - 10 of 48 pro vyhledávání: '"Yu. N. Chelnokov"'
3
Solution of the Problem of Optimal Spacecraft Launching into Orbit Using Reactive Acceleration and Solar Sail in Kustaanheimo–Stiefel Variables
Autor: Yu. N. Chelnokov, Ya. G. Sapunkov
Publikováno v: Cosmic Research. 59:280-290
Using the Pontryagin maximum principle and the Kustaanheimo–Stiefel variables, the spatial problem of optimal launching into a given orbit of a spacecraft (SC) controlled by a solar sail and limited or impulsive reactive acceleration of the SC’s
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::50583dcd69ffa2721ba612602486cb1a
https://doi.org/10.1134/s0010952521040055
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4
Controlling the Spatial Motion of a Rigid Body Using Biquaternions and Dual Matrices
Autor: Yu. N. Chelnokov
Publikováno v: Mechanics of Solids. 56:13-33
The method of analytical construction of the control of the spatial motion of a rigid body (control of screw motion, equivalent to the composition of angular (rotational) and translational movements) is being developed in a nonlinear dynamic setting
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::f530a9bd6f3d8d5c42a07af432d76cb9
https://doi.org/10.3103/s0025654421010064
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6
Synthesis of Control of Spatial Motion of a Rigid Body Using Dual Quaternions
Autor: Yu. N. Chelnokov
Publikováno v: Mechanics of Solids. 55:977-998
In this paper, we develop a new method of analytical design and control of the spatial motion of a rigid body (in particular, a spacecraft considered as a rigid body) in a nonlinear dynamic formulation using dual quaternions (Clifford biquaternions).
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::62a3c7aac1d78552d2e6703af6b8296f
https://doi.org/10.3103/s0025654420070080
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7
Regular Quaternion Models of Perturbed Orbital Motion of a Rigid Body in the Earth’s Gravitational Field
Autor: Yu. N. Chelnokov
Publikováno v: Mechanics of Solids. 55:958-976
In this paper, we propose regular quaternion models of perturbed orbital motion of a rigid body. They do not have the features inherent in classical models when a body moves in a Newtonian gravitational field and, in the general case, when a body mov
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::49e19cf2b90a16a4f6ef4516f4c42a8c
https://doi.org/10.3103/s0025654420070079
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8
Generalization of Hamilton–Ishlinskii Solid Angle Theorem for Spatial Motion of a Solid Body and its Applications
Autor: Yu. N. Chelnokov
Publikováno v: Mechanics of Solids. 54:1227-1239
Using the Kotelnikov–Study transference principle, a generalization of the Hamilton–Ishlinskii solid angle theorem for spatial motion of a solid that is a composition of translational and rotational motions and the dual conjugate theorem for the
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::bd1c3ba12cd7bd66efab31141b1e310f
https://doi.org/10.3103/s0025654419080132
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9
Quaternion Solution of the Problem of Optimal Rotation of the Orbit Plane of a Variable-Mass Spacecraft Using Thrust Orthogonal to the Orbit Plane
Autor: Yu. N. Chelnokov, Ya. G. Sapunkov
Publikováno v: Mechanics of Solids. 54:941-957
The problem of the optimal rotation of the orbital plane of a spacecraft (SC) of variable mass in an inertial coordinate system is solved in a nonlinear formulation using the quaternionic differential equation of orientation of the orbital coordinate
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::78a3877d813a3880e889c46d46def222
https://doi.org/10.3103/s0025654419060098
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10
Quaternion Models and Algorithms of Solving the General Problem of Energetically Optimal Spacecraft Orbit Reorientation
Autor: Ya. G. Sapunkov, Yu. N. Chelnokov, I. A. Pankratov
Publikováno v: Mekhatronika, Avtomatizatsiya, Upravlenie. 20:498-503
The problem of optimal reorientation of the spacecraft orbit is considered in quaternion formulation. Control (vector of the acceleration of the jet thrust) is limited in magnitude. It is required to determine the optimal orientation of the vector of
Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::f4aaec3fc286fb7bfba76ab980f36dc4
https://doi.org/10.17587/mau.20.498-503
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