FUZZY CONTROL OF RIGID SPACECRAFT ATTITUDE MANEUVER WITH DECAY RATE AND INPUT CONSTRAINTS

DOI10.1142/S0218488511007453zbMath1250.93076MaRDI QIDQ2919974

Xihai Zhang, Xiao Yu, Ming Zeng

Publication date: 23 October 2012

Published in: International Journal of Uncertainty, Fuzziness and Knowledge-Based Systems (Search for Journal in Brave)

zbMATH Keywords

fuzzy controlinput constraintsdecay rateTakagi-Sugeno modelspacecraft attitude

Mathematics Subject Classification ID

Fuzzy control/observation systems (93C42) Application models in control theory (93C95)

Uses Software

• Matlab
• LMI toolbox

Cites Work

• The attitude control problem
• Inverse optimal stabilization of a rigid spacecraft
• Robust attitude stabilization of spacecraft using nonlinear quaternion feedback
• Fuzzy Control for an Oceanic Structure: A Case Study in Time-delay TLP System
• ADAPTIVE FUZZY SLIDING MODE CONTROL FOR SEISMICALLY EXCITED BRIDGES WITH LEAD RUBBER BEARING ISOLATION

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