Zobrazeno 1 - 10
of 16
pro vyhledávání: '"G. L. Degtyarev"'
Publikováno v:
Russian Aeronautics. 65:561-567
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3e11d271257cd550129707a91b93ceab
https://doi.org/10.3103/s1068799822030151
https://doi.org/10.3103/s1068799822030151
Publikováno v:
Russian Aeronautics. 64:189-196
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b2c466831034a7c321504ad5b3acf50a
https://doi.org/10.3103/s1068799821020033
https://doi.org/10.3103/s1068799821020033
Publikováno v:
Russian Aeronautics. 63:604-609
The theory of vertical fall in the atmosphere was investigated as applied to an unmanned return spacecraft for various cases of ratio of the initial and quasi-steady-state velocities of fall. The modeling of the braking process, which is the numerica
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::77c557801c08869d8541d3663241aca6
https://doi.org/10.3103/s1068799820040066
https://doi.org/10.3103/s1068799820040066
Publikováno v:
Russian Aeronautics. 62:585-594
A technique of multiobjective robust controller synthesis for an electro-optical device line-of-sight stabilization system with saturating actuators is developed on the basis of polytopic linear parameter-varying system theory. From the computational
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3260c1178cdb90dbb766a198e1960af7
https://doi.org/10.3103/s1068799819040081
https://doi.org/10.3103/s1068799819040081
Analytical Design of the Law for Control of the Center of Mass Motion for an Unmanned Aerial Vehicle
Publikováno v:
Russian Aeronautics. 62:206-212
The control of the lift direction in space is considered. We synthesized the control of the mechanism of the center of mass motion in the longitudinal direction for regulating the static margin and in the transverse direction for creating the balanci
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::58147c7f56a1ab505380ec2543b05cd5
https://doi.org/10.3103/s1068799819020053
https://doi.org/10.3103/s1068799819020053
Publikováno v:
Mekhatronika, Avtomatizatsiya, Upravlenie. 19:691-698
In the paper multiobjective robust controller synthesis problem for nonlinear mechanical system described by Lagrange’s equations of the second kind is considered. Such tasks have numerous practical applications, for example in controller design of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::3cd699bd7d3c7439d1c9496e7476afa9
https://doi.org/10.17587/mau.19.691-698
https://doi.org/10.17587/mau.19.691-698
Publikováno v:
Russian Aeronautics. 61:541-546
A technique of multiobjective robust controller synthesis for airborne electro-optical device line-of-sight stabilization system is developed. The multiobjective synthesis of the robust control law for the stabilization system being considered is per
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2d0197c7207e74f258d92cee09a82b5e
https://doi.org/10.3103/s1068799818040062
https://doi.org/10.3103/s1068799818040062
Publikováno v:
Russian Aeronautics. 61:325-330
We present a design lay-out diagram of the reusable space transportation system that consists of an aerospace transformed vehicle that is injected into an orbit by means of the first and second stages. Some starting configurations of such system with
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::39944fd407e9973838313f1898615430
https://doi.org/10.3103/s1068799818030029
https://doi.org/10.3103/s1068799818030029
Publikováno v:
Russian Aeronautics. 61:23-31
Real values of parameters for a space vehicle and its steering devices are specified by using the motion parameters measured in flight based on solving the differential equations of motion.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::84328325016b2f9e26b6cde6345a8e3f
https://doi.org/10.3103/s106879981801004x
https://doi.org/10.3103/s106879981801004x
Publikováno v:
Russian Aeronautics. 60:349-357
In this paper, we introduce a concept of coordinated turn that means the application of the lifting force being perpendicular to the UAV velocity vector and parallel to the surface on which the exact point target is located. Analytical solutions of t
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::d2590f0f0dee677eabb6f1f94f37c6c9
https://doi.org/10.3103/s1068799817030059
https://doi.org/10.3103/s1068799817030059