Zobrazeno 1 - 10
of 10
pro vyhledávání: '"S. O. Karpenko"'
Publikováno v:
Acta Astronautica. 116:339-348
An analytical approach to study of attitude determination algorithms is considered. The approach is applicable for quasi-stationary motion determination. It is based on filter post-convergence computation of the Kalman filter covariance matrix and al
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::215435dc494897c9bd415567241cd88f
https://doi.org/10.1016/j.actaastro.2015.07.001
https://doi.org/10.1016/j.actaastro.2015.07.001
Publikováno v:
Acta Astronautica. 105:12-16
New one-axis magnetic attitude control is proposed. Only one attitude sensor providing any inertial direction measurements is necessary, magnetometer is not used. The control may be used as a backup capability in case main actuators or some attitude
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::305e5ba0d47d142bc1280edb94c464a8
https://doi.org/10.1016/j.actaastro.2014.08.017
https://doi.org/10.1016/j.actaastro.2014.08.017
Autor:
Danil Ivanov, M. Yu. Ovchinnikov, S. O. Karpenko, Dmitry Sergeevich Roldugin, N. A. Ivlev, Stepan Sergeevich Tkachev
Publikováno v:
Cosmic Research. 52:205-215
The attitude control system of the Chibis-M microsatellite is described. Results of flight experiments on damping the initial angular velocity (made using magnetorquers) are considered, as well as stabilization in the orbital referece frame, and orie
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::1703591026224f2c7fa442b04a865101
https://doi.org/10.1134/s0010952514020038
https://doi.org/10.1134/s0010952514020038
Autor:
A. V. Gurevich, G. A. Vladimirova, V. M. Kozlov, V. M. Gotlib, Natan Eysmont, Stanislav Klimov, A. A. Sukhanov, O. V. Batanov, V.N. Angarov, A. A. Lizunov, I. V. Yashin, P. Segedi, M. B. Dobriyan, A. P. Papkov, S. O. Karpenko, M. I. Panasyuk, N. A. Ivlev, Vladimir Nazarov, Anton Ledkov, S. I. Svertilov, A. V. Bogomolov, A. V. Kalyuzhnyi, M. S. Dolgonosov, Gali Garipov, L. Bodnar, V. N. Karedin, V.G. Rodin, I. V. Kozlov, V. V. Bogomolov, D. I. Vavilov, Ch. Ferenz, Valery Korepanov, Lev Zelenyi
Publikováno v:
Cosmic Research. 52:87-98
This paper describes the scientific goals and design developments of the Chibis microsatellite platform and the Groza scientific equipment, which are aimed at studying new physical mechanisms of high-altitude electrical discharges in the atmosphere.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::af2adf9a5f329d0db90315f3ff6cfa12
https://doi.org/10.1134/s0010952514010110
https://doi.org/10.1134/s0010952514010110
Autor:
Danil Ivanov, N. A. Ivlev, S. O. Karpenko, Stepan Sergeevich Tkachev, M. Yu. Ovchinnikov, Dmitry Sergeevich Roldugin
Publikováno v:
Acta Astronautica. 93:23-33
Design, analytical investigation, laboratory and in-flight testing of the attitude determination and control system (ADCS) of a microsatellites are considered. The system consists of three pairs of reaction wheels, three magnetorquers, a set of Sun s
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9a99885a7b6f969bb997e685ea157fa5
https://doi.org/10.1016/j.actaastro.2013.06.030
https://doi.org/10.1016/j.actaastro.2013.06.030
Publikováno v:
Cosmic Research. 51:478-484
An active magnetic control synthesis for attitude guidance of “Chibis-M” microsatellite is considered. The only information required is the data from the sun sensor. Applicability of a control to achieve solar panels sun-pointing is studied. Equa
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b1769d805fea266496f7b9f2775a4528
https://doi.org/10.1134/s0010952513060087
https://doi.org/10.1134/s0010952513060087
Publikováno v:
Cosmic Research. 50:431-440
We study the controlled angular motion of the Chibis-M microsatellite. Executive elements are three pairs of flywheels, whose axes are mutually perpendicular. The task of the control system is realization of a required program motion and support of i
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::586bd2b1f9f21b9d56526877dcd6ec9c
https://doi.org/10.1134/s0010952512060044
https://doi.org/10.1134/s0010952512060044
Publikováno v:
Cosmic Research. 50:170-176
We consider the rapid rotation of a satellite equipped with an active magnetic attitude control system with the -Bdot algorithm designed to damp the initial angular velocity. The time-response of the algorithm is analytically studied as a function of
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::e903af8f5efcb713325f0ae915ddf5b5
https://doi.org/10.1134/s0010952512010078
https://doi.org/10.1134/s0010952512010078
Autor:
S. O. Karpenko, Dmitry Sergeevich Roldugin, Stepan Sergeevich Tkachev, Danil Ivanov, M. Yu. Ovchinnikov
Publikováno v:
Journal of Computer and Systems Sciences International. 51:106-125
A laboratory facility developed at the Engineering Technological Center "Scan Ex" for testing algorithms for determination of attitude and stabilization of the attitude system of the satellite "Chibis-M" is described. The results of experiments on da
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::64e7e2f6b948b96d069ab8c4a7c6c595
https://doi.org/10.1134/s1064230711060104
https://doi.org/10.1134/s1064230711060104
Autor:
S. O. Karpenko, Oleg Evgen'evich Khromov, N. V. Kupriyanova, V. I. Pen’kov, M. Yu. Ovchinnikov, A. S. Selivanov
Publikováno v:
Cosmic Research. 48:517-525
The results of designing the attitude control system of the first Russian nanosatellite TNS-0 no. 1 providing orientation of its longitudinal axis along the local geomagnetic field induction vector are presented. The system consists of a permanent ma
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2273ecbc17fa7396f544bc37d5c50f91
https://doi.org/10.1134/s0010952510060043
https://doi.org/10.1134/s0010952510060043