Progress of Stewart Vibration Platform in Aerospace Micro–Vibration Control
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, characteri...
| Main Authors: | , , , , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
MDPI AG
2022-06-01
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| Series: | Aerospace |
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| Online Access: | https://www.mdpi.com/2226-4310/9/6/324 |
| _version_ | 1797491070066491392 |
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| author | Zepeng He Xiangchao Feng Yeqing Zhu Zhibo Yu Zhen Li Yan Zhang Yinhang Wang Pengfei Wang Liangyu Zhao |
| author_facet | Zepeng He Xiangchao Feng Yeqing Zhu Zhibo Yu Zhen Li Yan Zhang Yinhang Wang Pengfei Wang Liangyu Zhao |
| author_sort | Zepeng He |
| collection | DOAJ |
| description | 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. |
| first_indexed | 2024-03-10T00:42:02Z |
| format | Article |
| id | doaj.art-56bd9f6299cc4e98aadb80ba6a6ffdd2 |
| institution | Directory Open Access Journal |
| issn | 2226-4310 |
| language | English |
| last_indexed | 2024-03-10T00:42:02Z |
| publishDate | 2022-06-01 |
| publisher | MDPI AG |
| record_format | Article |
| series | Aerospace |
| spelling | doaj.art-56bd9f6299cc4e98aadb80ba6a6ffdd22023-11-23T15:05:46ZengMDPI AGAerospace2226-43102022-06-019632410.3390/aerospace9060324Progress of Stewart Vibration Platform in Aerospace Micro–Vibration ControlZepeng He0Xiangchao Feng1Yeqing Zhu2Zhibo Yu3Zhen Li4Yan Zhang5Yinhang Wang6Pengfei Wang7Liangyu Zhao8School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, ChinaQian Xuesen Laboratory of Space Technology, China Academy of Space Technology, Beijing 100094, ChinaSchool of Computer Science and Technology, Beijing Institute of Technology, Beijing 100081, ChinaIntelligent Equipment Division, Beijing Sunwise Intelligent Technology Co., Ltd., Beijing 100094, ChinaQian Xuesen Laboratory of Space Technology, China Academy of Space Technology, Beijing 100094, ChinaQian Xuesen Laboratory of Space Technology, China Academy of Space Technology, Beijing 100094, ChinaQian Xuesen Laboratory of Space Technology, China Academy of Space Technology, Beijing 100094, ChinaQian Xuesen Laboratory of Space Technology, China Academy of Space Technology, Beijing 100094, ChinaSchool of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, ChinaIn 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.https://www.mdpi.com/2226-4310/9/6/324spacecraftmicro–vibrationvibration isolation technologyStewart platformactive and passive integration |
| spellingShingle | Zepeng He Xiangchao Feng Yeqing Zhu Zhibo Yu Zhen Li Yan Zhang Yinhang Wang Pengfei Wang Liangyu Zhao Progress of Stewart Vibration Platform in Aerospace Micro–Vibration Control Aerospace spacecraft micro–vibration vibration isolation technology Stewart platform active and passive integration |
| title | Progress of Stewart Vibration Platform in Aerospace Micro–Vibration Control |
| title_full | Progress of Stewart Vibration Platform in Aerospace Micro–Vibration Control |
| title_fullStr | Progress of Stewart Vibration Platform in Aerospace Micro–Vibration Control |
| title_full_unstemmed | Progress of Stewart Vibration Platform in Aerospace Micro–Vibration Control |
| title_short | Progress of Stewart Vibration Platform in Aerospace Micro–Vibration Control |
| title_sort | progress of stewart vibration platform in aerospace micro vibration control |
| topic | spacecraft micro–vibration vibration isolation technology Stewart platform active and passive integration |
| url | https://www.mdpi.com/2226-4310/9/6/324 |
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