Variable structure robust flight control system for the F-14

IEEE Transactions on Aerospace and Electronic Systems

Volumn 33, Issue 1, 1997, Pages 77-84

  Singh, Sahjendra N ^a   Steinberg, Marc ^a   Digirolamo, Robert D ^a  

^a University of Nevada Las Vegas   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; AIRCRAFT MODELS; CLOSED LOOP CONTROL SYSTEMS; COMPUTER SIMULATION; CONTROL SYSTEM SYNTHESIS; ERRORS; FLIGHT DYNAMICS; LINEAR CONTROL SYSTEMS; MATHEMATICAL MODELS; MULTIVARIABLE CONTROL SYSTEMS; TRACKING (POSITION); VELOCITY CONTROL;

FLIGHT CONTROL LAW; FLIGHT CONTROL SYSTEM; LATERAL VELOCITY; M INPUT Q OUTPUT LINEAR UNCERTAIN SYSTEMS; PARAMETER UNCERTAINTY; ROLL ANGLE; SLIDING SURFACE; TRACKING ERROR; VARIABLE STRUCTURE CONTROL THEORY; YAW RATE;

CONTROL THEORY;

EID: 0030735518     PISSN: 00189251     EISSN: None     Source Type: Journal    
DOI: 10.1109/7.570710     Document Type: Article

References (13)

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