TY - JOUR
T1 - On low-complexity control design to spacecraft attitude stabilization
T2 - An online-learning approach
AU - Zhang, Chengxi
AU - Xiao, Bing
AU - Wu, Jin
AU - Li, Bo
N1 - Publisher Copyright:
© 2020 Elsevier Masson SAS
PY - 2021/3
Y1 - 2021/3
N2 - This paper studies the spacecraft attitude stabilization problem with external disturbances. A new control scheme entitled online-learning control is proposed to achieve a robust, accurate, and simple-structure control algorithm. Compared with the conventional control design, an obvious distinction of the online-learning control algorithm is that it together utilizes the previous control input information and the system's current state information, as if learning experience from previous control input. In contrast, the conventional control scheme does not fully use the existing information and chooses to discard the previous control input information when generating control instructions. Due to the learning strategy, the utility of adaptive- or observer-based tools can be avoided when designing a robust control law, making a simple, effective algorithm, moreover saving system resources. The proposed control law can stabilize the attitude system by achieving the uniformly ultimately bounded convergence.
AB - This paper studies the spacecraft attitude stabilization problem with external disturbances. A new control scheme entitled online-learning control is proposed to achieve a robust, accurate, and simple-structure control algorithm. Compared with the conventional control design, an obvious distinction of the online-learning control algorithm is that it together utilizes the previous control input information and the system's current state information, as if learning experience from previous control input. In contrast, the conventional control scheme does not fully use the existing information and chooses to discard the previous control input information when generating control instructions. Due to the learning strategy, the utility of adaptive- or observer-based tools can be avoided when designing a robust control law, making a simple, effective algorithm, moreover saving system resources. The proposed control law can stabilize the attitude system by achieving the uniformly ultimately bounded convergence.
KW - Attitude stabilization
KW - Online-learning control (OLC)
KW - Spacecraft control
UR - http://www.scopus.com/inward/record.url?scp=85099189906&partnerID=8YFLogxK
U2 - 10.1016/j.ast.2020.106441
DO - 10.1016/j.ast.2020.106441
M3 - 文章
AN - SCOPUS:85099189906
SN - 1270-9638
VL - 110
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 106441
ER -