Adaptive linear parameter varying control synthesis for actuator failure

Journal of Guidance, Control, and Dynamics

Volumn 27, Issue 5, 2004, Pages 787-794

  Shin, Jong Yeob ^a   Wu, N Eva ^b,d   Belcastro, Christine ^c,e  

^a NATIONAL INSTITUTE OF AEROSPACE   (United States)

^b BINGHAMTON UNIVERSITY   (United States)

^c NASA LANGLEY RESEARCH CENTER   (United States)

^d Department of Electrical Engineering ^*

^e Guidance Control Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; ERROR DETECTION; FAILURE ANALYSIS; FAULT TOLERANT COMPUTER SYSTEMS; LINEAR CONTROL SYSTEMS; MANEUVERABILITY; OPTIMIZATION;

ACTUATOR FAILURE; ADAPTIVE LINEAR PARAMETER VARYING (ALPV); CONTROL SYNTHESIS; HIGHLY MANEUVERABLE AIRCRAFT TECHNOLOGY (HIMAT);

ACTUATORS;

EID: 4944235126     PISSN: 07315090     EISSN: 15333884     Source Type: Journal    
DOI: 10.2514/1.9430     Document Type: Article

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