Research on Attitude Maneuver and Vibration of Liquid-filled Flexible Spacecraft Based on Terminal Sliding Mode Control

Author:

WU Taotao,SONG Xiaojuan,LÜ Shufeng

Publisher

National Space Science Center, Chinese Academy of Sciences

Subject

General Medicine

Reference24 articles.

1. REYHANOGLU M, HERVAS J R. Robotically controlled sloshing suppression in point-to-point liquid container transfer[J]. Journal of Vibration and Control, 2013, 19(14): 2137-2144

2. SONG Xiaojuan, WANG Hongwei, YUE Baozeng. Adaptive robust fault tolerant control of liquid-filled spacecraft with measurement uncertainty[J]. Journal of Astronautics, 2022, 43(5): 638-648
宋晓娟, 王宏伟, 岳宝增. 测量不确定的充液航天器自适应鲁棒容错控制[J]. 宇航学报, 2022, 43(5): 638-648

3. DENG M L, YUE B Z. Attitude dynamics and control of liquid filled spacecraft with large amplitude fuel slosh[J]. Journal of Mechanics, 2017, 33(1): 125-136

4. DENG Mingle, YUE Baozeng, HUANG Hua. Study on the equivalent mechanical model for large amplitude slosh[J]. Journal of Astronautics, 2016, 37(6): 631-638
邓明乐, 岳宝增, 黄华. 液体大幅晃动类等效力学模型研究[J]. 宇航学报, 2016, 37(6): 631-638

5. NAVABI M, DAVOODI A, REYHANOGLU M. Optimum fuzzy sliding mode control of fuel sloshing in a spacecraft using PSO algorithm[J]. Acta Astronautica, 2020, 167: 331-342

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