跳到主要导航
跳到搜索
跳到主要内容
西北工业大学 国内
English
中文
国内
简介
研究单位
科研成果
按专业知识、名称或附属进行搜索
Non-fragile negative imaginary output feedback control for attitude stabilization of flexible spacecraft
Ziyu Yang, Chuang Liu,
Xiaokui Yue
, Ming Guo
航天学院
Northwestern Polytechnical University Xian
CAS - Innovation Academy for Microsatellites
科研成果
:
期刊稿件
›
文章
›
同行评审
8
引用 （Scopus）
综述
指纹
指纹
探究 'Non-fragile negative imaginary output feedback control for attitude stabilization of flexible spacecraft' 的科研主题。它们共同构成独一无二的指纹。
分类
加权
按字母排序
Engineering
Feedback Control
100%
Output Feedback
100%
Flexible Spacecraft
100%
Model Parameter
66%
Parameter Uncertainty
66%
Control System
33%
Actuator
33%
Flexible Structures
33%
Attitude Control
33%
Closed Loop
33%
External Disturbance
33%
Vibration Control
33%
Iterative Algorithm
33%
H-Performance
33%
Controller Gain
33%
Inequality Constraint
33%
Computer Science
Parameter Uncertainty
100%
output feedback control
100%
Output Feedback
50%
actuator fault
50%
Iterative Algorithm
50%
Numerical Simulation
50%
linear matrix
50%
Inequality Constraint
50%
Vibration Control
50%