Adaptive fuzzy attitude control of satellite based on linearization

Proceedings of the American Control Conference

Volumn 2, Issue , 2004, Pages 1091-1096

  Guan, P ^a   Liu, X J ^b   Lara Rosano, F ^b   Chen, J B ^a  

^a BEIJING INSTITUTE OF TECHNOLOGY   (China)

^b UNIVERSIDAD NACIONAL AUTÓNOMA DE MÉXICO   (Mexico)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; EQUATIONS OF MOTION; LINEARIZATION; MATRIX ALGEBRA; PROBLEM SOLVING; ROBUSTNESS (CONTROL SYSTEMS); SATELLITES; VECTORS;

MULTI-INPUT MULTI-OUTPUT (MIMO); REACTION JETS; VARIABLE STRUCTURE CONTROL;

FUZZY CONTROL;

EID: 8744312539     PISSN: 07431619     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.23919/acc.2004.1386717     Document Type: Conference Paper

References (4)

1. N. S. Sahjendra and Y. Woosoon, "Feedback linearization and solar pressure satellite attitude control," IEEE Trans. on aerospace and electronic systems, vol.32, no.2, pp.732-741, 1996.
2. N. S. Sahjendra and I. Ashok, "Nonlinear decoupling sliding mode control and attitude control of spacecraft," IEEE Trans. on aerospace and electronic systems, vol.25, no.5, pp.621-633, 1989.
3. H. Elmali and N. Olgac, "Robust output tracking of MIMO nonlinear systems via sliding mode technique," Automatic, vol.28, no.1, pp.145-151, 1992.
4. H. Elmali and N.Olgac, "Satellite attitude control via sliding mode with perturbation estimation," IEE Proc.-control theory application, vol.143, no.3, pp.276-282, 1996.