Nonlinear H∞ optimal control for agile missiles

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 1, 1996, Pages 157-165

  Wise, Kevin A ^a,b,c,d,e   Sedwick, Jack L ^a,d,f  

^a BOEING COMPANY   (United States)

^b McDonnell Douglas Aerospace East

^c University of Missouri Rolla   (United States)

^d SOUTHERN ILLINOIS UNIVERSITY EDWARDSVILLE   (United States)

^e UNIVERSITY OF ILLINOIS AT URBANA CHAMPAIGN   (United States)

^f WASHINGTON UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; APPROXIMATION THEORY; COMPUTER SIMULATION; FLIGHT DYNAMICS; MATHEMATICAL MODELS; MISSILES; NONLINEAR CONTROL SYSTEMS; PARTIAL DIFFERENTIAL EQUATIONS;

AGILE MISSILES; HAMILTON JACOBI ISAACS EQUATION; PITCH PLANE FLIGHT CONTROL SYSTEM;

OPTIMAL CONTROL SYSTEMS;

EID: 0029756723     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21593     Document Type: Article

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