Reconfigurable control of aircraft in nonlinear flight regimes

Collection of Technical Papers - AIAA Guidance, Navigation, and Control Conference

Volumn 4, Issue , 2005, Pages 3220-3230

  Chang, Bor Chin ^a,e,f   Kwatny, Harry G ^a,e,f   Thomas, Suba ^b,f,g   Bajpai, Gaurav ^b,f,g   Hu, Daniel Chunlong ^c,h   Belcastro, Christine ^d,f,i  

^a DREXEL UNIVERSITY   (United States)

^b TECHNO SCIENCES INC   (United States)

^c Kulicke and Soffa Industries Inc   (United States)

^d NASA LANGLEY RESEARCH CENTER   (United States)

^e MEM Department   (United States)

^f AIAA   (United States)

^g Processing Engineering Group ^*  (United States)

^h Processing Engineering Group   (United States)

ⁱ Dynamic Systems and Control Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MODELS; BIFURCATION (MATHEMATICS); CONTROL THEORY; FAILURE ANALYSIS; FLIGHT DYNAMICS; MULTIVARIABLE CONTROL SYSTEMS;

F-16 AIRCRAFT; NASA LANGLEY RESEARCH CENTER; NONLINEAR FLIGHT REGIMES; RECONFIGURABLE CONTROL OF AIRCRAFT;

AIRCRAFT;

EID: 29744449178     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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