航天器工程2019，Vol.28Issue(6)：15-23,9.DOI:10.3969/.j issn.1 673-8748.2019.06.003
基于主被动一体隔振指向平台的柔性航天器高精高稳指向方法
Method of Flexible Spacecraft High Precision and Stability Pointing Based on Active-passive Integrated Vibration Isolation and Pointing Platform
摘要
Abstract
To satisfy increasingly high precision and stability pointing requirements of future as-tronomical satellites and remote sensing satellites,and solve the contradictions between pointing control and vibration suppression,the paper proposes a method to achieve high precision and sta-bility pointing of flexible spacecraft by introducing a Stewart platform with abilities of both vibra-tion suppression and pointing control.The dynamics model of the whole satellite with Stewart platform and flexible appendages is established and active-passive integrated controller is designed.Simulation of transmissibility is done and the pointing control performance of the Stew-art platform is analyzed by numerical simulation.The results show that the platform can meet the demand of vibration isolation and pointing adj ustment at the same time,which can provide a refer-ence for future development of high pointing performance spacecraft.关键词
主被动一体/Stewart平台/隔振/高精高稳指向Key words
active-passive integration/Stewart platform/vibration isolation/high precision and stability pointing分类
航空航天引用本文复制引用
徐广德,田蕾,邓凯文,吴冬梅,张柏楠,孙国童,张永..基于主被动一体隔振指向平台的柔性航天器高精高稳指向方法[J].航天器工程,2019,28(6):15-23,9.基金项目
国家重大科技专项工程 （）
