A SIMPLIFIED MODEL FOR VIBRATING MASS CONTROL MOMENT GYROSCOPE

Date

2017-02-09

Author

Akbulut, Burak
Arberkli, Ferhat
Azgın, Kıvanç
Tekinalp, Ozan

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This work is licensed under a Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License.

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A novel satellite attitude actuator based on vibrating masses was previously proposed. Its governing equations were obtained and simulated. In this study, the resulting mathematical model is validated via energy as well as the conservation of angular momentum methods. Additionally, the mathematical model for the complete system was too complicated for analysis. In this work, a representative simplified set of equations describing vibrating mass control moment gyroscope (vCMG) dynamics in high fidelity are also obtained . It is shown that the simplified model may be used to simulate the complex vCMG dynamics under certain conditions.

Subject Keywords

Spacecraft

URI

https://hdl.handle.net/11511/55729

Conference Name

27th AAS/AIAA Space Flight Mechanics Meeting

Collections

Department of Mechanical Engineering, Conference / Seminar

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Citation Formats

B. Akbulut, F. Arberkli, K. Azgın, and O. Tekinalp, “A SIMPLIFIED MODEL FOR VIBRATING MASS CONTROL MOMENT GYROSCOPE,” San Antonio, TX, 2017, vol. 160, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/55729.