Method for Justification of Requirements to the Angular Field of View of an Opto-Electronic Instrument of a Space Robot for Measuring Motion Parameters of an Orbital Object
https://doi.org/10.17586/0021-3454-2024-67-11-969-974
Abstract
The problem of refining the center of mass motion parameters of a non-cooperating spacecraft using an optical unit for measuring the spacecraft angular position relative to two navigation stars is considered. The article presents the results of development of a methodology for substantiating the requirements for the angular field of view of an optical electronic instrument installed on board a service space robot to measure the motion parameters of a non-cooperative spacecraft subject to maintenance.
About the Authors
A. D. Golyakov
A. F. Mozhaisky Military Space Academy
Russian Federation
Russian Federation
Alexey D. Golyakov — Dr. Sci., Professor; Department
of Autonomous Control Systems
A. A. Sasunkevich
A. F. Mozhaisky Military Space Academy
Russian Federation
Russian Federation
Aleksander A. Sasunkevich — PhD; Department of
Autonomous Control Systems; Doctoral Cand.
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For citations:
Golyakov A.D., Sasunkevich A.A. Method for Justification of Requirements to the Angular Field of View of an Opto-Electronic Instrument of a Space Robot for Measuring Motion Parameters of an Orbital Object. Journal of Instrument Engineering. 2024;67(11):969-974. (In Russ.) https://doi.org/10.17586/0021-3454-2024-67-11-969-974
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