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

Authors: 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
Affiliations:
1. Moscow Experimental Design Bureau “Mars”
Issue: Vol 50, No 7 (2016)
Pages: 540-545
Section: Article
URL: https://journal-vniispk.ru/0038-0946/article/view/170591
DOI: https://doi.org/10.1134/S0038094616070224
ID: 170591

Cite item

Full Text

Open Access
Restricted Access

Access granted
Restricted Access

Subscription Access

Abstract
About the authors
References
Supplementary files
Statistics

Abstract

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.