This work presents an approach for satellite control systems incorporating the flexibility of components and their vibrations during maneuvers. The structures that are not considered rigid bodies are modelled by finite elements as to determine their first natural modes. These results are applied to approximate the complete system in the Assumed Modes Method and to derive the equations of motion through the Lagrangian mechanics.
This work presents an approach for satellite control systems incorporating the flexibility of components and their vibrations during maneuvers. The structures that are not considered rigid bodies are modelled by finite elements as to determine their first natural modes. These results are applied to approximate the complete system in the Assumed Modes Method and to derive the equations of motion through the Lagrangian mechanics.
Equations of motion and passive vibration control for flexible satellites
MEYER de OREY GAIVÃO, LUIS FELIPE
2018/2019
Abstract
This work presents an approach for satellite control systems incorporating the flexibility of components and their vibrations during maneuvers. The structures that are not considered rigid bodies are modelled by finite elements as to determine their first natural modes. These results are applied to approximate the complete system in the Assumed Modes Method and to derive the equations of motion through the Lagrangian mechanics.| File | Dimensione | Formato | |
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MeyerDeOreyGaivao.pdf
Open Access dal 14/05/2021
Descrizione: Thesis text
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https://hdl.handle.net/10589/154428