Multidisciplinary optimization framework for control-configuration integration in aircraft conceptual design

Journal of Aircraft

Volumn 43, Issue 6, 2006, Pages 1937-1948

  Perez, Ruben E ^a,c,d   Liu, Hugh H T ^a,c,d   Behdinan, Kamran ^b,d,e  

^a UNIVERSITY OF TORONTO   (Canada)

^b RYERSON UNIVERSITY   (Canada)

^c Institute for Aerospace Studies   (Canada)

^d AIAA   (United States)

^e Department of Aerospace Engineering ^*

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING; CONTROL SYSTEM ANALYSIS; COST EFFECTIVENESS; FLIGHT DYNAMICS; OPTIMIZATION; STRUCTURAL DESIGN;

AIRCRAFT DESIGN; COMMERCIAL AIRCRAFTS; CONTROL INTEGRATION; FLIGHT ENVELOPE;

AEROSPACE VEHICLES;

EID: 33846177912     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.22263     Document Type: Article

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