Adaptive actuator failure compensation designs for a linearized aircraft longitudinal model

AIAA Guidance, Navigation, and Control Conference and Exhibit

Volumn , Issue , 2002, Pages

  Chen, Shuhao ^a   Tao, Gang ^a   Josh, Suresh M ^b  

^a University of Virginia   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ACTUATORS; AIRCRAFT; CONTROL SURFACES; LINEARIZATION; STATE FEEDBACK;

ACTUATOR FAILURES; ADAPTIVE ACTUATOR; AIRCRAFT FLIGHT CONTROL; LONGITUDINAL DYNAMICS; LONGITUDINAL MODELS; OUTPUT FEEDBACK DESIGN; PERFORMANCE DEGRADATION; STATE-FEEDBACK DESIGNS;

FLIGHT CONTROL SYSTEMS;

EID: 85086488769     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-4438     Document Type: Conference Paper

References (11)

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