期刊文献+
共找到1篇文章
< 1 >
每页显示 20 50 100
Singularity analysis for single gimbal control moment gyroscope system using space expansion method 被引量:4
1
作者 Yunhua WU Feng HAN +2 位作者 Bing HUA Zhiming CHEN Feng YU 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2018年第4期782-794,共13页
Control Moment Gyroscope(CMG) is an effective candidate for agile satellites and large spacecraft attitude control because of its powerful torque amplification capability. The most serious situation, however, in usi... Control Moment Gyroscope(CMG) is an effective candidate for agile satellites and large spacecraft attitude control because of its powerful torque amplification capability. The most serious situation, however, in using CMG is the inherent geometric singularity problem, where there's no torque output along a particular direction. Space expansion method has been proposed in this work for the singularity analysis. Based on inverse mapping transformation, an expanded Jacobian matrix which is a full rank square matrix is obtained. The singular angle sets of the 3-parallel cluster and pyramid cluster are distinguished using space expansion method. An effective hybrid steering strategy, able to deal with the elliptic singularity, is further proposed. Simulation results demonstrate the excellent performance of the proposed steering logic compared to the generalized singular robust logic and pseudo inverse logic in terms of energy consumption and torque error. 展开更多
关键词 agile spacecraft Control moment gyro Singularity analysis Space expansion method Steering strategy
原文传递
上一页 1 下一页 到第
使用帮助 返回顶部