Fuzzy control based on H∞ output feedback for attitude stabilization of flexible satellite

IEEE International Conference on Fuzzy Systems

Volumn 1, Issue , 2001, Pages 159-162

  Nam, Sae Kyu ^a   Kim, Kyung Keun ^a  

^a Agency for Defence Development   (South Korea)

Author keywords

[No Author keywords available]

Indexed keywords

CONTROL SYSTEM SYNTHESIS; FEEDBACK CONTROL; LINEAR CONTROL SYSTEMS; MULTIVARIABLE CONTROL SYSTEMS; NONLINEAR CONTROL SYSTEMS; OPTIMIZATION; ROBUSTNESS (CONTROL SYSTEMS); SATELLITES; SYSTEM STABILITY;

ATTITUDE STABILIZATION; FLEXIBLE SATELLITE; ROBUST FUZZY MULTI-VARIABLE CONTROLLER;

FUZZY CONTROL;

EID: 0035747009     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. An augmented Lagrangian method for a class of LMI- Constrained problems in robust control theory
2. An approach to fuzzy control of nonlinear systems: Stability and design issues
3. ∞ fuzzy output feedback control design for nonlinear dynamic systems: An LMI approach
4. Fuzzy identification of system and its application to modeling and control
5. ∞ control of uncertain fuzzy continuous-time systems
6. Robust fuzzy control of a magnetic bearing system subject to harmonic disturbances
7. Comparison of low-earth-orbit satellite attitude controllers submitted to controllability constraints
8. Fuzzy multi-variable control for attitude stabilization of flexible spacecraft
9. Fuzzy PID control with accelerated reasoning for d. c. servo motors