Review of reaction spheres for spacecraft attitude control

被引:24
作者
Zhu, Linyu [1 ]
Guo, Jian [1 ]
Gill, Eberhard [1 ]
机构
[1] Delft Univ Technol, Fac Aerosp Engn, NL-2629 HS Delft, Netherlands
关键词
Actuator; Motors; Bearings; PERMANENT-MAGNET ACTUATOR; SPHERICAL ULTRASONIC MOTOR; FINITE-ELEMENT-METHOD; STEPPING MOTOR; OF-FREEDOM; FIELD COMPUTATION; REACTION WHEEL; DESIGN; TORQUE; BEARING;
D O I
10.1016/j.paerosci.2017.04.001
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
With respect to spacecraft attitude control, reaction spheres are promising alternatives to conventional momentum exchange devices for the benefits brought by their 4 pi rotation. Many design concepts of reaction spheres have been proposed in the past decades, however, developments of the driving unit and the bearing, as well as their combination remain great challenges. To facilitate research and push developments in this field, this paper provides a comprehensive review of reaction spheres. To some extent, an in-depth survey of multi-DOF (degree of freedom) spherical motors and possible bearings is provided, along with their advantages and weaknesses addressed. Some multi-DOF actuators for different applications, such as robotic joints, are investigated since they share many similar challenges and techniques with reaction spheres. The experimental performances of realized reaction spheres are listed and compared. Limits of current designs are identified and their causes are analyzed and discussed. Compared with existing summaries on multi-DOF actuators and some surveys done for specific reaction spheres' design, this paper provides the first thorough review on reaction spheres, considering approaches to excite and support the free 4 pi rotation.
引用
收藏
页码:67 / 86
页数:20
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