Nonlinear control theory for a class of structural nonlinearities in a prototypical wing section

35th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1997, Pages

  Ko, Jeonghwan ^a   Kurdila, Andrew J ^a   Strganac, Thomas W ^a  

^a Texas AandM University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROELASTICITY; AEROSPACE ENGINEERING; CLOSED LOOP CONTROL SYSTEMS; CONTROL NONLINEARITIES; CONTROL THEORY; FEEDBACK LINEARIZATION; NONLINEAR FEEDBACK; SYSTEM STABILITY;

ADAPTIVE CONTROL METHODS; ASYMPTOTICALLY STABLE; CLOSED LOOP STABILITY; NONLINEAR CONTROL LAWS; NONLINEAR CONTROL THEORY; PARTIAL FEEDBACK LINEARIZATION; PROTOTYPICAL WING SECTION; STRUCTURAL NON-LINEARITIES;

ADAPTIVE CONTROL SYSTEMS;

EID: 84983212264     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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