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Output feedback robust H
∞
control for spacecraft rendezvous system subject to input saturation: A gain scheduled approach
Yi Huang
, Yingmin Jia
*
*
Corresponding author for this work
Beihang University
Research output
:
Contribution to journal
›
Article
›
peer-review
13
Citations (Scopus)
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Dive into the research topics of 'Output feedback robust H
∞
control for spacecraft rendezvous system subject to input saturation: A gain scheduled approach'. Together they form a unique fingerprint.
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Engineering
Output Feedback
100%
Space Rendezvous
100%
Control Scheme
66%
Computer Simulation
33%
State Information
33%
Stability Analysis
33%
Gain Control
33%
Parameter Uncertainty
33%
Feedback Gain
33%
Gain Controller
33%
Convergence Performance
33%
Riccati Equation
33%
Gain Matrix
33%
Capacity Control
33%
Scheduled Controller
33%