交叉簧片柔性虎克铰在静平衡仪中的应用及性能测试
收稿日期: 2015-03-12
修回日期: 2015-09-30
网络出版日期: 2022-03-17
基金资助
国家自然科学基金(51105014, 51275017)和教育部博士点基金(2011 1102130004)资助项目
Received date: 2015-03-12
Revised date: 2015-09-30
Online published: 2022-03-17
通过对广义交叉簧片柔性铰链转角公式的分析，揭示了铰链刚度和仪器灵敏度之间的关系。为了避免垂直载荷的变化对铰链转动刚度的影响，设计具有恒定转动刚度的交叉簧片柔性虎克铰，并以柔性虎克铰为转动支撑单元搭建针对万向节装置不平衡力矩测量的两自由度柔性静平衡仪。通过对沿特定方向特定量不平衡力矩的测量，在0～7
张述卿 , 毕树生 , 赵宏哲 , 宗光华 , 刘浪 . 交叉簧片柔性虎克铰在静平衡仪中的应用及性能测试[J]. 机械工程学报, 2015 , 51(21) : 1 -6 . DOI: 10.3901/JME.2015.21.001
The relationship between instrument sensitivity and rotational stiffness of the pivot is revealed by analyzing the rotational stiffness equation of the cross-spring pivot. In order to eliminate the impacts of payload changes on instrument sensitivity, a cross-spring Hooke hinge with constant rotational stiffness is designed as the rotation unit of a 2-DOF static balancing instrument for unbalanced moment measurement of gimbaled devices. Certain amount of unbalance moments along certain direction are measured by the instrument and the synchronization sensitivity along x axis and y axis is investigated. Experimental results show that when the payload ranges from
[1] SCHWARTZ J L，PECK M A，HALL C D. Historical review of air-bearing spacecraft simulators[J]. Journal of Guidance，Control，and Dynamics，2003，26(4)：513-522.
[2] KARAMI M A，SASSANI F. Spacecraft momentum dumping using fewer than three external control torques[J]. Journal of Guidance，Control，and Dynamics，2009，32(1)：242-247.
[3] BAE J，KIM Y. Adaptive controller design for spacecraft formation flying using sliding mode controller and neural networks[J]. Journal of the Franklin Institute，2012，349(5)：578-603.
[4] REYNERSON，CHARLES M. Aerodynamic disturbance force and torque for spacecraft and simple shapes using finite plate elements - Part II：Aerodynamic force & torque[C]// 2012 IEEE Aerospace Conference，March 3-10，2012，Big Sky，MT，United States，2012：1-9.
[5] SANYAL A，FOSBURY A，CHATURVEDI N. Inertia-free spacecraft attitude tracking with disturbance rejection and almost global stabilization[J]. Journal of Guidance，Control，and Dynamics，2009，32(4)：1167-1178.
[6] SAM W. Parameter estimation of a spacecraft simulator using parameter-adaptive control[D]. Blacksburg：Virginia Polytechnic and State University，2006.
[7] MARK L，PSIAKI. Estimation of the parameters of a spacecraft’s attitude dynamics model using flight data[J]. Journal of Guidance，Control，and Dynamics，2005，28(4)：594-603.
[8] 陈欢龙，周军，刘莹莹. 多体卫星物理仿真动态调平衡干扰力矩分析[J]. 计算机仿真，2010，27(10)：66-70. CHEN Huanlong，ZHOU Jun，LIU Yingying. Analysis of disturbance torque on multi-body satellite physical simulation[J]. Computer Simulation，2010，27(10)：66-70.
[9] 向东，杨庆俊，包钢，等.三轴气浮平台常值干扰力矩的分析与补偿[J]. 宇航学报，2009，30(2)：448-452. XIANG Dong，YANG Qingjun，BAO Gang，et al. Research on analysing and compensation of the steady disturbing torque of the three axis air bearing table[J]. Journal of Astronautics，2009，30(2)：448-452.
[10] 林来兴. 试论气浮台仿真的功能[J]. 控制工程，1983(4)：1-9. LIN Laixing. Study on the function of the air-bearing table simulation[J]. Control Engineering of China，1983(4)：1-9.
[11] 李季苏，牟小刚，孙维德. 大型卫星三轴气浮台全物理仿真系统[J]. 控制工程，2001，3：22-26. LI Jisu，MOU Xiaogang，SUN Weide. Large three-axis physical simulation for satel-lite control systems[J]. Control Engineering of China，2001，3：22-26.
[13] 李延斌，杨庆俊，王祖温. 3自由度气浮台力学性能研究——自重作用对转动惯量矩阵及惯量主轴方向的影响[J]. 机械工程学报，2006，42(4)：191-195. LI Yanbin，YANG Yingjun，WANG Zuwen.Study on the mechanics property of three degrees of freedom air-bearing testbed——Influence on the moment of inertia matrix and on the direction of inertia principal axis when acted on gravity[J]. Chinese Journal of Mechanical Engineering，2006，42(4)：191-195.
[14] 李延斌，王祖温，包钢，等. 3自由度气浮台力学性能研究——自重作用下平台结构平衡敏感性分析[J]. 机械工程学报，2008，44(11)：310-316. LI Yanbin，WANG Zuwen，BAO Gang，et al. Study on the mechanics property of three degrees of freedom air-bearing testbed——equilibrium sensitivity analysis of the platform structure acted on gravity[J]. Chinese Journal of Mechanical Engineering，2008，44(11)：310-316.
[15] YU Jinying，ZHAO Keding，
[16] HUANG Qitao，JIANG Hongzhou，ZHANG Shangying，et al. Spacecraft docking simulation using hardware-in- the-loop simulator with stewart platform[J]. Chinese Journal of Mechanical Engineering，2005，18(3)：415-418.
[17] KIM J J，AGRAWAL B N. Automatic mass balancing of air-bearing-based three-axis rotational spacecraft simulator[J]. Journal of Guidance Control and Dynamic，2009，32(3)：1005-1007.
[18] 戴路，金光.三轴姿态控制仿真系统快速自动精确调平方法研究及仿真[J].清华大学学报，2011，51(8)：1063-1071. DAI Lu，JIN Guang.Research and simulation on a method for automatic mass balancing of a 3-aixs attitude control test bed[J]. J. Tsinghua Univ.，2011，51(8)：1063-1071.
[19] ROMANO M，AGRAWAL B N. Acquisition，tracking and pointing control of the bifocal relay mirror spacecraft[J]. Acta Astronautica，2003，53：509-519.
[20] PRADO J，BISIACCHI G，REYES L，et al. Three-axis air-bearing based platform for small satellite attitude determination and control simulation[J]. Journal of Applied Research and Technology，2005，3(3)：222-237.
[21] SCHWARTZ J L. The distributed spacecraft attitude control systems simulator：From design concept to decentralized control[D]. Blacksburg：Virginia Polytechnic Institute and State Univeristy，2004.
/
| 〈 |
|
〉 |