Finite-time attitude tracking control for spacecraft using terminal sliding mode and chebyshev neural network

IEEE Transactions on Systems, Man, and Cybernetics, Part B: Cybernetics

Volumn 41, Issue 4, 2011, Pages 950-963

  Zou, An Min ^a   Kumar, Krishna Dev ^a   Hou, Zeng Guang ^b   Liu, Xi ^a  

^a RYERSON UNIVERSITY   (Canada)

^b INSTITUTE OF AUTOMATION   (China)

Author keywords

Adaptive control; attitude tracking; Chebyshev neural network (NN) (CNN); spacecraft; terminal sliding mode (TSM)

Indexed keywords

ADAPTIVE CONTROL; ADAPTIVE NEURAL CONTROL; APPROXIMATION ERRORS; ATTITUDE TRACKING; ATTITUDE TRACKING CONTROL; BASIS FUNCTIONS; CHEBYSHEV NEURAL NETWORK (NN) (CNN); CHEBYSHEV NEURAL NETWORKS; CONTROL INPUT CONSTRAINTS; DESIRED SIGNAL; DOUBLE INTEGRATOR; ERROR DYNAMICS; EXTERNAL DISTURBANCES; FINITE TIME STABILITY; GLOBAL REPRESENTATION; HYPERBOLIC TANGENT FUNCTION; MASS MOMENT; NN CONTROL; NONLINEAR FUNCTIONS; ROBUST CONTROLLERS; SLIDING MANIFOLDS; SPACECRAFT ATTITUDE; SWITCH FUNCTION; TERMINAL SLIDING MODE; TERMINAL SLIDING MODE (TSM);

CONTROLLERS; HYPERBOLIC FUNCTIONS; NAVIGATION; NEURAL NETWORKS;

SPACECRAFT;

EID: 79960700479     PISSN: 10834419     EISSN: None     Source Type: Journal    
DOI: 10.1109/TSMCB.2010.2101592     Document Type: Article

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