FAULT TOLERANCE OF SPACECRAFT ORIENTATION AND STABILIZATION SYSTEM
DOI:
https://doi.org/10.15588/1607-3274-2013-2-17Keywords:
stabilization and orientation spacecraft system, fault tolerance, reaction wheel, angular velocity sensor.Abstract
Formed the structure of the orientation and stabilization system for ensuring its active fault tolerance. Parameterized types of failures of the system functional elements, characterized by changes in the properties of the conversion elements. Received diagnostic functional models for solving problems of detection, search the place and establish a class of failure for system. Developed models and methods of systematic approach to fault tolerance in the direction of the effective use of the signal, parametric and structural redundancies and selection of parrying tools. Performed experimental researches of the sample model of the automatic attitude control and stabilization the properties of active fault-tolerance in emergency modes of operation.References
Alekseev Yu. S., Belous E. V., Belyaev G. V. i dr./ pod obshhej red. Alekseeva Yu. S., Zlatkina Yu. M., Krivcova V. S., Kulika A. S., Chumachenko V. I. Proektirovanie i e’ksperimental’naya otrabotka sistem upravleniya ob”ektov raketno-kosmicheskoj texniki. T. 2. Proektirovanie sistem upravleniya kosmicheskix apparatov i modulej orbital’nyx stancij [Tekst]: uchebnik v 3 t. Har’kov: Nac. ae’rokosm. un-t im. N. E. Zhukovskogo «Xar’k. aviac. in-t», NPP Xartron-Arkos, 2012, 680 p.
Kulik A. S., Luchenko O. A., Firsov S. N. Algoritmicheskoe obespechenie modulej diagnostirovaniya i vosstanovleniya rabotospsosbnosti sputnikovoj sistemy orientacii i stabilizacii [Tekst], Radio Electronics, Computer Science, Control, 2012, No. 1 (26), pp. 112–122.
Postnikov V. N., Taran A. N., Firsov S. N. Kriterii ocenki svojstv izbytochnyx maxovichnyx sistem [Tekst], Radioelektronni ta kompiuterni systemy, 2011, No. 4 (52), pp. 82–87.
Kulik A. S., Luchenko O. A., Firsov S. N. Koncepciya obespecheniya zhivuchesti sputnikovyx sistem upravleniya orientaciej i stabilizaciej, Radio Electronics, Computer Science, Control, 2011, No. 2 (25), pp. 41–47.
Kulik A. S., Subbota A. M., Reznikova O. V. E’ffektivnost’ izbytochnyx sistem stabilizacii i orientacii kosmicheskix apparatov s dvigatelyami-maxovikami [Tekst], Aviacionnokosmicheskaya texnika i texnologiya, 2008, No. 3 (50), pp. 18–25.
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Copyright (c) 2014 S. N. Firsov, O. V. Reznikova
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