Attitude dynamics simulation and analysis of a flexible satellite
Abstract Dynamic models of flexible satellites are carried out using the virtual work principle. The kinematic model and the dynamic model are established respectively. The coupling characteristics of the flexible mechanism and its influence on the attitude of the satellite are analyzed by simulation, and the correctness of the mathematical modeling is validated.
Authors
- Yonghe Zhang (ORCID: https://orcid.org/0000-0002-3817-8694)
- Danfeng Liu
- Wen Chen (ORCID: https://orcid.org/0000-0002-7821-0791)
- Heng Zhou
- Yingquan Yang
- Jinsong Li (ORCID: https://orcid.org/0000-0003-3456-662X)
Institutions
- Shanghai Micro Satellite Engineering Center (CN)
- Shanghai Jian Qiao University (CN)
- Innovation Academy for Microsatellites of Chinese Academy of Sciences
Publication Details
- Journal
- Journal of Physics Conference Series
- Published
- 2024-08-01
- DOI
- https://doi.org/10.1088/1742-6596/2820/1/012047
- Citations
- 1
- Primary Topic
- Dynamics and Control of Mechanical Systems
- Type
- article
- Field-Weighted Citation Impact
- 0.33