Discrete-time, mixed-norm control synthesis applied to aircraft terrain following

Journal of Guidance, Control, and Dynamics

Volumn 19, Issue 5, 1996, Pages 1088-1094

  Jacques, David R ^a,b,c   Ridgely, D Brett ^a,c   Canfield, Robert A ^a,c  

^a AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

^c AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

CONSTRAINT THEORY; DISCRETE TIME CONTROL SYSTEMS; FIGHTER AIRCRAFT; MATHEMATICAL MODELS; OPTIMAL CONTROL SYSTEMS; OPTIMIZATION; ROBUSTNESS (CONTROL SYSTEMS); SYSTEM STABILITY; TRANSFER FUNCTIONS;

COMPLEMENTARY SENSITIVITY; DISCRETE TIME LINEAR SYSTEMS; MIXED NORM CONTROL SYNTHESIS; TERRAIN FOLLOWING PROBLEM;

CONTROL SYSTEM SYNTHESIS;

EID: 0030241003     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/3.21749     Document Type: Article

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