Design Parameters Selection for CubeSat Nanosatellite with a Passive Stabilization System
https://doi.org/10.17285/0869-7035.0025
Abstract
Probabilistic study of angular motion dynamics has been performed for CubeSat nanosatellites with passive stabilization systems, including aerodynamic, aerodynamicgravitational, gravitational, and gravitational-aerodynamic ones. Analytical functions of the maximum angle values distribution have been obtained for a nanosatellite axes deviation from required directions (orbital velocity vector or a local vertical) for uniform distribution and Rayleigh distribution of the component values of the initial angular rate vector. Formulas have been derived and bunch graphs have been plotted for selecting the design parameters (geometrical dimensions, static stability margin, moments of inertia) which ensure the required attitude with the specified probability in circular orbits.
About the Authors
I. V. Belokonov
S.P. Korolev Samara National Research University,
Samara, Russia
Russian Federation
Russian Federation
I. A. Timbai
S.P. Korolev Samara National Research University,
Samara, Russia
Russian Federation
Russian Federation
E. V. Barinova
S.P. Korolev Samara National Research University,
Samara, Russia
Russian Federation
Russian Federation
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Review
For citations:
Belokonov I.V., Timbai I.A., Barinova E.V. Design Parameters Selection for CubeSat Nanosatellite with a Passive Stabilization System. Giroskopiya i Navigatsiya. 2020;28(1):81-100. (In Russ.) https://doi.org/10.17285/0869-7035.0025
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