An Observer-Based Anti-unwinding Attitude Control Method for Flexible Spacecraft

Author:

Yuan Binwen,Dong Rui-QiORCID,Yang DengORCID

Publisher

Springer Nature Singapore

Reference16 articles.

1. He, G., Cao, D.: Dynamic modeling and attitude-vibration cooperative control for a large-scale flexible spacecraft. Actuators 12(4), Art no. 167 (2023)

2. Golestani, M., Zhang, W., Yang, Y., Xuan-Mung, N.: Disturbance observer-based constrained attitude control for flexible spacecraft. IEEE Trans. Aerosp. Electron. Syst. 59(2), 963–972 (2023)

3. Huo, J.: Research on the high-precision and agile attitude control system for micro-nano satellite with complex structure. PH. D. dissertation, School of Aeronautics and Astronautics, Zhejiang Univ., Hangzhou, Zhejiang (2020)

4. Ma, G., Xu, M., Tian, J., Kan, X.: The vibration suppression of solar panel based on smart structure. Aeronaut. J. 125(1283), 244–255 (2021)

5. Zhu, C., Sun, H., Hou, L.: Anti-disturbance attitude quantized control of flexible spacecraft via a triggering and quantization joint dynamic event-triggered mechanism. Aerospace Science and Technology 136, Art no. 108191 (2023)

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