| 基于双力源的叠加式多维力传感器校准装置研究CSCD |
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| 引用本文： | 邓松波,刘小勇,李科,刘书选,王燕波. 基于双力源的叠加式多维力传感器校准装置研究CSCD[J]. 宇航计测技术, 2015, 38(6): 38-43. DOI: 10.12060/j.issn.1000-7202.2018.06.07 |
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| 作者姓名： | 邓松波 刘小勇 李科 刘书选 王燕波 |
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| 作者单位： | 1、北京精密机电控制设备研究所，北京 100076;;2、中国人民解放军火箭军驻长征航天控制工程公司军事代表室，北京 100076 |
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| 基金项目： | 中国运载火箭技术研究院产业发展基金(MJK-1686-04) |
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| 摘 要： | 介绍了一种基于叠加机原理的双力源多维力传感器校准装置的设计与研制,对装置的测量不确定度进行了分析,通过对三分量力传感器的校准实验,证明了校准装置不仅可以对多分量力传感器进行单分量校准,还能方便地实现耦合误差的校准。
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| 关 键 词： | 多维力传感器 标定 校准装置 |
A Position and Attitude Tracking Method Research for Air Bearing Simulator |
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| DENG Song-bo,LIU Xiao-yong,LI Ke,LIU Shu-xuan,WANG Yan-bo. A Position and Attitude Tracking Method Research for Air Bearing Simulator[J]. Journal of Astronautic Metrology and Measurement, 2015, 38(6): 38-43. DOI: 10.12060/j.issn.1000-7202.2018.06.07 |
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| Authors: | DENG Song-bo LIU Xiao-yong LI Ke LIU Shu-xuan WANG Yan-bo |
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| Affiliation: | 1、Beijing Research Institute of Precise Mechanical and Electronic Control Equipment, Beijing 100076,China;;2、Military Representative Office of The Rocket Force in Long March Aerospace Controling Engineering Company of China Academy of Launch Vehicle Technology, Beijing 100076,China |
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| Abstract: | In order to simulate the attitude motion and orbital maneuvering motion of the space vechicle in ground state, the air bearing spacecraft simulator would be moved in large plane and angle space. To make the actual orbit and attitude movement of the simulator to form the closed-loop control, it is needed to provide a method to measure the position and attitude of the simulator in rapid way and high precision. The iGPS is used to measure the position of the simulator, while the SINS to attitude. The air propulsion devices and the reaction wheels are used as the servo motion to realize the position and attitude tracking. It could be widely applied in other environments of large scale space position and attitude measurement tracking. |
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| Keywords: | Air bearing simulator iGPS Inertial navigation Position and attitude tracking Space vehicle |
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