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Analysis of the influence of low-orbit nanosatellite uncontrolled motion on the possibility of solving navigation and communication problems after its separation from the «Soyuz» carrier rocket upper-stage
- Authors: Belokonov I.V.1, Kramlikh A.V.1, Timbai I.A.1
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Affiliations:
- Samara State Aerospace University
- Issue: Vol 12, No 4 (2013)
- Pages: 76-85
- Section: ISSUE WITHOUT SECTION
- URL: https://journals.ssau.ru/vestnik/article/view/25
- DOI: https://doi.org/10.18287/1998-6629-2013-0-4(42)-76-85
- ID: 25
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Abstract
The paper analyses a nanosatellite’s uncontrolled motion relative to its mass center after separation from the upper stage of «Soyuz» carrier rocket. Stochastic models of the initial conditions of the nanosatelite attitude motion are formulated. The possibility of successful solutions of navigation and communication problems using satellite navigation systems and low-altitude communications networks for LEO nanosatellites is shown.
About the authors
I. V. Belokonov
Samara State Aerospace University
Author for correspondence.
Email: acad@ssau.ru
Doctor of Engineering, Professor
Head of Space Research Department
Russian FederationA. V. Kramlikh
Samara State Aerospace University
Email: kramlikh@mail.ru
Candidate of Engineering
Associate Professor of the Department of Space Mechanical Engineering
Russian FederationI. A. Timbai
Samara State Aerospace University
Email: timbai@ssau.ru
Doctor of Engineering Science
Professor of the Department of Higher Mathematics
Russian FederationReferences
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