Aircraft nonminimum phase control in dynamic sliding manifolds

Journal of Guidance, Control, and Dynamics

Volumn 24, Issue 3, 2001, Pages 566-572

  Shkolnikov, I A ^a   Shtessel, Y B ^a  

^a UNIVERSITY OF ALABAMA IN HUNTSVILLE   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ALGORITHMS; APPROXIMATION THEORY; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; EIGENVALUES AND EIGENFUNCTIONS; ERROR ANALYSIS; FLIGHT DYNAMICS; MATHEMATICAL MODELS; NONLINEAR CONTROL SYSTEMS; PHASE CONTROL; POLYNOMIALS;

DYNAMIC SLIDING MANIFOLDS; MULTI INPUT MULTI OUTPUT SYSTEMS; NONMINIMUM PHASE OUTPUT TRACKING; PIECEWISE POLYNOMIAL SPLINE MODEL;

SLIDING MODE CONTROL;

EID: 0035334470     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/2.4747     Document Type: Article

References (21)

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