The onboard control system of “Navigator” platform

A. S. Syrov; V. V. Smirnov; V. N. Sokolov; G. S. Iodko; V. V. Mischikhin; V. N. Kosobokov; M. A. Shatskii; D. A. Dobrynin

doi:10.1134/S0038094616070224

The onboard control system of “Navigator” platform

作者: Syrov A.S.¹, Smirnov V.V.¹, Sokolov V.N.¹, Iodko G.S.¹, Mischikhin V.V.¹, Kosobokov V.N.¹, Shatskii M.A.¹, Dobrynin D.A.¹
隶属关系:
1. Moscow Experimental Design Bureau “Mars”
期: 卷 50, 编号 7 (2016)
页面: 540-545
栏目: Article
URL: https://journals.rcsi.science/0038-0946/article/view/170591
DOI: https://doi.org/10.1134/S0038094616070224
ID: 170591

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详细

A brief description of the design concept, structure and performance of the onboard control system (AOCS) of the “Navigator” satellite platform, on the basis of which the spacecraft “Electro-L’ and “Spektr-R” are designed, is presented. The test-flight results of the AOCS attitude accuracy are given. Approaches to the further development of the onboard control equipment for advanced spacecraft are determined and presented.