Modeling of the Deployment Process Dynamics for Large-Sized Transformable Space Structures

Modeling of the Deployment Process Dynamics for Large-Sized Transformable Space Structures

A dynamic model of the deployment of the large-sized transformable space structures (by the example of solar panels) is proposed. The model is based on using the Lagrange equations of the second kind. The model capabilities are illustrated by calculation results of the main integral parameters chara...

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Veröffentlicht in:Russian aeronautics 2020-12, Vol.63 (4), p.610-617
Hauptverfasser: Bakulin, V. N., Borzykh, S. V.
Format: Artikel
Sprache:eng
Schlagworte:
Automotive Engineering
Engineering
Flight Dynamics and Control of Flight Vehicles
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Beschreibung
Zusammenfassung:A dynamic model of the deployment of the large-sized transformable space structures (by the example of solar panels) is proposed. The model is based on using the Lagrange equations of the second kind. The model capabilities are illustrated by calculation results of the main integral parameters characterizing the solar panel deployment process.
ISSN:1068-7998
1934-7901
DOI:10.3103/S1068799820040078