Analysis of the influence of the error of the nanosatellite design and dynamic performances on the quality of angular motion control processes

By the nanosatellite angular motion control in this research is meant terminal control based on inverse dynamics problem solution using the Bellman's optimality principle. The impact of the error of the nanosatellite design and dynamic performances, which are torques of inertia, attitude angles...

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Bibliographic Details
Published in:IOP conference series. Materials Science and Engineering 2020-11, Vol.984 (1), p.12016
Main Authors: Belokonov, I V, Kramlikh, A V, Melnik, M E
Format: Article
Language:English
Subjects:
Angular velocity
Inverse dynamics
Motion control
Nanosatellites
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Summary:By the nanosatellite angular motion control in this research is meant terminal control based on inverse dynamics problem solution using the Bellman's optimality principle. The impact of the error of the nanosatellite design and dynamic performances, which are torques of inertia, attitude angles and angular rates, on the quality of angular motion control processes (i.e. on the accuracy of its reorientation), is investigated. The results of numerical simulation are given through the example of the nanosatellite of the SamSat family.
ISSN:1757-8981
1757-899X
DOI:10.1088/1757-899X/984/1/012016