DocumentCode
613670
Title
Rapid concept development of the mission space architecture, process modeling, and capability analysis
Author
Flanigan, Daniel ; Schneider, B. ; Wolfrom, J.
Author_Institution
Johns Hopkins Univ. Appl. Phys. Lab., Laurel, MD, USA
fYear
2013
fDate
15-18 April 2013
Firstpage
504
Lastpage
511
Abstract
Early system engineering is not focused on the natural triangle of relationships between architecture, alternatives and performance. As a result, early understanding of conceptual trade space is focused on a sequential and independent effort when developing the system concept. This method is rife with inefficiency, broad and incorrect assumptions of the preceding step, ultimately leading to large amounts of rework and a non-unifying effort throughout the project team. This paper provides a means to show through an illustrative example that these three elements are interconnected and building them simultaneously improves the efficiency of concept development. The results of the paper highlight the parallel relationships between the elements that are usually developed in a serial process. This method provides the means to continuously build related architecture, alternatives, and performance elements together.
Keywords
aerospace; systems engineering; capability analysis; conceptual trade space; mission space architecture; process modeling; rapid concept development; system engineering; Computer architecture; Jamming; Mathematical model; Meteorology; Modeling; Space missions; model based systems engineering; systems analysis; systems architecture;
fLanguage
English
Publisher
ieee
Conference_Titel
Systems Conference (SysCon), 2013 IEEE International
Conference_Location
Orlando, FL
Print_ISBN
978-1-4673-3107-4
Type
conf
DOI
10.1109/SysCon.2013.6549929
Filename
6549929
Link To Document