×
验证码:
换一张
忘记密码?
记住我
CORC
首页
科研机构
检索
知识图谱
申请加入
托管服务
登录
注册
在结果中检索
科研机构
长春光学精密机械与物... [3]
内容类型
期刊论文 [2]
会议论文 [1]
发表日期
2022 [1]
2019 [1]
2010 [1]
×
知识图谱
CORC
开始提交
已提交作品
待认领作品
已认领作品
未提交全文
收藏管理
QQ客服
官方微博
反馈留言
浏览/检索结果:
共3条,第1-3条
帮助
限定条件
专题:长春光学精密机械与物理研究所
第一署名单位
第一作者单位
通讯作者单位
已选(
0
)
清除
条数/页:
5
10
15
20
25
30
35
40
45
50
55
60
65
70
75
80
85
90
95
100
排序方式:
请选择
作者升序
作者降序
题名升序
题名降序
发表日期升序
发表日期降序
提交时间升序
提交时间降序
Neural network-based continuous finite-time tracking control for uncertain robotic systems with actuator saturation
期刊论文
Asian Journal of Control, 2022, 卷号: 24, 期号: 6, 页码: 3475-3493
作者:
Y. Li
;
H. Y. Sai
;
M. C. Zhu
;
Z. B. Xu and D. Q. Mu
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2023/06/14
Vector Control-Based Singularity Avoidance/Escape Steering Law for Single Gimbal Control Moment Gyros
期刊论文
Ieee Access, 2019, 卷号: 7, 页码: 175727-175743
作者:
N.Mao
;
T.Zhang
;
K.Xu
;
M.S.Chen
;
C.Dong
收藏
  |  
浏览/下载:1/0
  |  
提交时间:2020/08/24
Steering law,SGCMG,satellite attitude control,logic,spacecraft,sgcmg,Computer Science,Engineering,Telecommunications
United steering of control moment gyros for small satellite with limited gimbal rate (EI CONFERENCE)
会议论文
2010 IEEE International Conference on Information and Automation, ICIA 2010, June 20, 2010 - June 23, 2010, Harbin, Heilongjiang, China
Xu K.
;
Jin G.
;
Chen C.
收藏
  |  
浏览/下载:15/0
  |  
提交时间:2013/03/25
Single Gimbal Control Moment Gyroscopes (SGCMG) can could provide large control torque and quick attitude maneuver rate to small satellites without any increase in power
volume and mass
which will help small satellites become more powerful. Singularity avoidance and failure steering are two important problems to SGCMGs and also the main focus in this field. A new united steering law for SGCMGs with capabilities of singularity avoidance and quick transition of singularity surfaces is developed in this paper. To ensuring the existence of null motion
the commanded output of controller was changed real-timely as the variation of singularity measurement of SGCMGs
which can avoid the gimbal angle rate saturation. This developed steering law could help the SGCMGs provide real-time control toques in spite of limitation of gimbal angle rate. Simulation analysis is conducted for a certain 4-SGCMG system mounted on a small satellite. Simulation results indicate that the steering law is very effective in singularity avoidance. 2010 IEEE.
©版权所有 ©2017 CSpace - Powered by
CSpace