The necessity of introducing a geometric control subsystem into the composite attitude control systems of spacecraft and aircraft with modern precision

M. E. Prokhorov; A. I. Zakharov; O. Yu. Stekolshchikov; M. S. Tuchin; M. K. Abubekerov; A. O. Zhukov

doi:10.1134/S1028335816010079

The necessity of introducing a geometric control subsystem into the composite attitude control systems of spacecraft and aircraft with modern precision

Authors: Prokhorov M.E.¹, Zakharov A.I.¹, Stekolshchikov O.Y.¹, Tuchin M.S.¹, Abubekerov M.K.¹, Zhukov A.O.¹
Affiliations:
1. Sternberg Astronomical Institute
Issue: Vol 61, No 1 (2016)
Pages: 5-7
Section: Physics
URL: https://journals.rcsi.science/1028-3358/article/view/190853
DOI: https://doi.org/10.1134/S1028335816010079
ID: 190853

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Abstract

We propose to introduce a geometric control subsystem into the attitude control systems of space-craft that would allow the current system sensor configuration to be determined in real time.