Development of an integrated aeroelastic multibody morphing simulation tool

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 5, Issue , 2006, Pages 3658-3667

  Reich, Gregory W ^a,c   Bowman, Jason C ^a   Sanders, Brian ^a,c   Frank, Geoffrey J ^b,c,d  

^a AIR FORCE RESEARCH LABORATORY   (United States)

^b UNIVERSITY OF DAYTON   (United States)

^c AIAA   (United States)

^d AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; COMPUTER SIMULATION; MATHEMATICAL MODELS; WINGS;

MORPHING AIRCRAFTS; VEHICLE MORPHING;

FLIGHT DYNAMICS;

EID: 34147156239     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-1892     Document Type: Conference Paper

References (8)

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8. Doman, D. B. and Oppenheimer, M. W., "Reconfigurable Control Design for the X-40A with In-Flight Simulation Results," AIAA 2004-5017, AIAA Guidance, Navigation, and Control Conference, Providence, Rhode Island, 16-19 August 2004.