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.
Modeling of the Deployment Process Dynamics for Large-Sized Transformable Space Structures
Russ. Aeronaut.
Russian Aeronautics ; 63 , 4 ; 610-617
2020-12-01
8 pages
Article (Journal)
Electronic Resource
English
Mathematical modeling of the deployment of a large transformable space structure
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