TY - JOUR
T1 - Progress of Stewart Vibration Platform in Aerospace Micro–Vibration Control
AU - He, Zepeng
AU - Feng, Xiangchao
AU - Zhu, Yeqing
AU - Yu, Zhibo
AU - Li, Zhen
AU - Zhang, Yan
AU - Wang, Yinhang
AU - Wang, Pengfei
AU - Zhao, Liangyu
N1 - Publisher Copyright:
© 2022 by the authors. Licensee MDPI, Basel, Switzerland.
PY - 2022/6
Y1 - 2022/6
N2 - In order to support the development of high–precision spacecraft, the current state of the Stewart vibration isolation platform in the field of aerospace micro–vibration was surveyed. First, based on analyses of the causes and characteristics of spacecraft micro–vibration, the principles, characteristics, advantages and disadvantages of four vibration isolation technologies are summarized. Second, the development process of the Stewart vibration isolation platform, from structural proposal and theoretical calculation to application in various fields, is introduced. Then, the current state of kinematics, dynamics and braking control algorithms of the Stewart platform is investigated, and related work on rigid/flexible platforms in the field of aerospace micro–vibration is introduced in detail. Finally, the idea that the Stewart platform can be fabricated by 4D printing technology is proposed. The novel Stewart platform can be combined with artificial intelligence algorithms and advanced control strategies, allowing for further development in the direction of an integrated omnidirectional, full–frequency and multi–function platform with variable stiffness.
AB - In order to support the development of high–precision spacecraft, the current state of the Stewart vibration isolation platform in the field of aerospace micro–vibration was surveyed. First, based on analyses of the causes and characteristics of spacecraft micro–vibration, the principles, characteristics, advantages and disadvantages of four vibration isolation technologies are summarized. Second, the development process of the Stewart vibration isolation platform, from structural proposal and theoretical calculation to application in various fields, is introduced. Then, the current state of kinematics, dynamics and braking control algorithms of the Stewart platform is investigated, and related work on rigid/flexible platforms in the field of aerospace micro–vibration is introduced in detail. Finally, the idea that the Stewart platform can be fabricated by 4D printing technology is proposed. The novel Stewart platform can be combined with artificial intelligence algorithms and advanced control strategies, allowing for further development in the direction of an integrated omnidirectional, full–frequency and multi–function platform with variable stiffness.
KW - Stewart platform
KW - active and passive integration
KW - micro–vibration
KW - spacecraft
KW - vibration isolation technology
UR - http://www.scopus.com/inward/record.url?scp=85132745774&partnerID=8YFLogxK
U2 - 10.3390/aerospace9060324
DO - 10.3390/aerospace9060324
M3 - Review article
AN - SCOPUS:85132745774
SN - 2226-4310
VL - 9
JO - Aerospace
JF - Aerospace
IS - 6
M1 - 324
ER -