自动化学报（英文版）2020，Vol.7Issue(2)：472-481,10.
Robust Adaptive Attitude Control for Non-rigid Spacecraft With Quantized Control Input
Robust Adaptive Attitude Control for Non-rigid Spacecraft With Quantized Control Input
Yun Li 1Fan Yang2
作者信息
- 1. Tandon School of Engineering, New York University, New York 11201 USA
- 2. Beijing National Research Center for Information Science and Technology (BNRist), the Department of Automation, Tsinghua University, Beijing 100084, China
- 折叠
摘要
关键词
Adaptive control/attitude control/input quantiza-tion/spacecraft/time-varying inertial parameterKey words
Adaptive control/attitude control/input quantiza-tion/spacecraft/time-varying inertial parameter引用本文复制引用
Yun Li,Fan Yang..Robust Adaptive Attitude Control for Non-rigid Spacecraft With Quantized Control Input[J].自动化学报（英文版）,2020,7(2):472-481,10.
