A framework for morphing capability assessment

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

Volumn 2, Issue , 2004, Pages 1582-1592

  Cesnik, Carlos E S ^a   Last, Howard R ^b   Martin, Christopher A ^b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b INSTITUTE FOR DEFENSE ANALYSES   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR VEHICLE MORPHING; MORPHING CONCEPT ASSESSMENT; MULTI-VARIABLE MISSIONS; SPACE MISSIONS;

COSTS; INVESTMENTS; RESEARCH AND DEVELOPMENT MANAGEMENT; SPACE RESEARCH; TECHNICAL PRESENTATIONS; TECHNOLOGY TRANSFER;

AEROSPACE VEHICLES;

EID: 16244380180     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (4)

1. "ONR/DARPA In-Flight Reconfigurable Aircraft Workshop (Report for Workshop Held at IDA, 10-11 December 2002)", Draft IDA Document D-2876 (in preparation).
2. Clough, B. T., "Metrics, schmetrics! How do you track a UAV's autonomy?," AIAA-2002-3499.
3. Boeing Corporation, "AFTI/F-111 Mission Adaptive Wing Briefing to Industry", AFWAL-TR-88-3082, October 1988.
4. Comstock, T., and K. Dooley, "A Tale of Two QFDs", Quality Management Journal. 5(4): 32-45, 1998