Robust nonlinear control for bank to turn missile

Proceedings of the World Congress on Intelligent Control and Automation (WCICA)

Volumn 4, Issue , 2002, Pages 2973-2977

  Zhang, Youan ^a   Yang, Huadong ^a   Hu, Yunan ^a  

^a NAVAL AERONAUTICAL AND ASTRONAUTICAL UNIVERSITY   (China)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DEGREES OF FREEDOM (MECHANICS); DYNAMICS; FEEDBACK CONTROL; LINEAR CONTROL SYSTEMS; LYAPUNOV METHODS; MISSILES; NONLINEAR CONTROL SYSTEMS; ROBUSTNESS (CONTROL SYSTEMS); STATE ESTIMATION; UNCERTAIN SYSTEMS; VELOCITY CONTROL;

AERODYNAMIC FORCE COEFFICIENTS; BANK TO TURN MISSILE; FAST STATES DYNAMICS; FEEDBACK LINEARIZATION THEORY; ROBUST NONLINEAR CONTROL; SIX DEGREES OF FREEDOM SIMULATION; SLOW STATES DYNAMICS;

CONTROL SYSTEM SYNTHESIS;

EID: 0036946751     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. J.H. Kim and J.S. Jang, "Nonlinear model inversion control for bank-to-turn missile", AIAA-95-3318-CP.
2. ∞ control with gain scheduling and dynamic inversion", J. Guid. Contr. Dyn., vol.21, no.2, 1998, pp. 234-243.
3. C.S. Chumacher, and P.P. Khargonekar, "Stability analysis of a missile control system with a dynamic inversion controller", J. Guid. Contr. Dyn., vol.21, no.3, 1998, pp. 508-514.
4. M.M. Polycarpou, "Stable adaptive neural network control scheme for nonlinear systems", IEEE Transactions on Automatic Control, vol.41, no.3, 1996, pp.447-451.