| 一种十二自由度航天模拟器对接性能试验装置 | |
| Alternative Title | Twelve 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
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| 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 | 31107 上海航天局专利中心 |
| Country | 中国 |
| Subtype | 发明授权 |
| 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 Abstract | The 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 | 否 |
| Application Date | 2017-09-14 |
| 2018-04-03 | |
| Date Available | 2020-06-26 |
| Application Number | CN201710826967.9 |
| Open (Notice) Number | CN107867414B |
| Language | 中文 |
| Contribution Rank | 2 |
| Document Type | 专利 |
| Identifier | http://ir.sia.cn/handle/173321/27288 |
| Collection | 智能产线与系统研究室 |
| Affiliation | 1.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. |
| Files in This Item: | ||||||
| File Name/Size | DocType | Version | Access | License | ||
| CN201710826967.9授权.p（1079KB） | 专利 | 开放获取 | CC BY-NC-SA | View Application Full Text | ||
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