DocumentCode
724002
Title
Deployment process control of space masts via iterative learning control
Author
Yangmin Xie ; Chao Xie ; Hang Shi
Author_Institution
Shanghai Key Lab. of Intell. Manuf. & Robot., Shanghai Univ., Shanghai, China
fYear
2015
fDate
23-25 May 2015
Firstpage
1026
Lastpage
1031
Abstract
The paper presents the initial study on the deployment control of the deployable tube-boom mast, a novel design concept of large space masts. The work first analyzes the deploying dynamics of the mast structure and identifies the issues of the free deployment in structural mechanics, which motivates the application of active process control. A data-driven iterative learning controller (ILC) is then proposed to function as an offline control signal trainer so that the well-trained deploying process could be able to track the desired smooth and slow trajectory and reduce the deployment-induced vibrations. To improve the computation efficiency, a sliding window method is incorporated in ILC to shorten the time period of trails for the control signal training iterations. Numerical investigation is carried out on a single boom of the deployable mast, showing the satisfactory trajectory tracking performance and strong capability for low-frequency dynamics attenuation. As the first application of ILC methods in the field of deployable structures, such results demonstrate that the proposed method is feasible to reform the deploying process of the deployable mast structure with enhanced structural stability and reliability.
Keywords
aerospace instrumentation; iterative learning control; process control; reliability theory; trajectory control; ILC method; active process control; computation efficiency; control signal training iteration; data-driven iterative learning controller; deployable structure; deployable tube-boom mast; deployment process control; deployment-induced vibration; design concept; free deployment; low-frequency dynamics attenuation; mast structure; numerical investigation; offline control signal trainer; satisfactory trajectory tracking performance; sliding window method; space mast; structural mechanics; structural reliability; structural stability; well-trained deploying process; Aerospace electronics; Computational efficiency; Fasteners; Process control; Space missions; Trajectory; Vibrations; Data Driven Control; Deployable Mast; Deployment Control; Iterative Learning Control; Space Structure;
fLanguage
English
Publisher
ieee
Conference_Titel
Control and Decision Conference (CCDC), 2015 27th Chinese
Conference_Location
Qingdao
Print_ISBN
978-1-4799-7016-2
Type
conf
DOI
10.1109/CCDC.2015.7162068
Filename
7162068
Link To Document