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一种十二自由度航天模拟器对接性能试验装置
Alternative TitleTwelve degree freedom flight simulator performance test device
张玉花; 徐志刚2; 胡震宇; 郑云青; 朱雪龙; 王治易; 李洪波; 俞旦; 倪波; 刘洲; 贺云2; 刘勇2
Department装备制造技术研究室
Rights Holder上海宇航系统工程研究所 ; 中国科学院沈阳自动化研究所
Patent Agent上海航天局专利中心 31107
Country中国
Subtype发明
Status有权
Abstract本发明提供一种十二自由度航天模拟器对接性能试验装置,包括二维平动驱动单元、主动偏航驱动单元、被动偏航驱动单元、主动航天模拟器和被动航天模拟器;主、被动偏航驱动单元分别设置于二维平动驱动单元两端,主动航天模拟器设置于主动偏航驱动单元上,被动航天模拟器设置于被动偏航驱动单元上;主动偏航驱动单元带动主动航天模拟器,模拟对接机构的主动端;被动偏航驱动单元和被动航天模拟器,模拟对接机构的被动端;本发明航天模拟器各自由度之间运动耦合性小,各自由度实现灵敏、可靠,运动范围大,运动轨迹不受限制,采用气浮技术模拟精度高。
Other AbstractThe device has an active yaw drive unit (2) and a passive yaw driving unit (3) fixed on the two-dimensional translational motion drive unit (1). Two ends of a driving simulator (4) are fixed on the active yaw driving unit. A driven flight simulator (5) is fixed on the passive yaw drive unit. A driven flight simulator simulates movement of a spacecraft through a built-in vertical weightless motion unit to realize vertical weightlessness movement freedom. A built-in motion physical attribute matching unit simulates rolling and pitch freedom of the spacecraft.
PCT Attributes
Application Date2017-09-14
2018-04-03
Date Available2020-06-26
Application NumberCN201710826967.9
Open (Notice) NumberCN107867414A
Language中文
Contribution Rank2
Document Type专利
Identifierhttp://ir.sia.cn/handle/173321/21926
Collection智能产线与系统研究室
Affiliation1.上海宇航系统工程研究所
2.中国科学院沈阳自动化研究所
Recommended Citation
GB/T 7714
张玉花,徐志刚,胡震宇,等. 一种十二自由度航天模拟器对接性能试验装置[P]. 2018-04-03.
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