DocumentCode :
1934648
Title :
Model-based verification and validation of the SMAP uplink processes
Author :
Khan, M.O. ; Dubos, G.F. ; Tirona, J. ; Standley, S.
Author_Institution :
Jet Propulsion Lab., California Inst. of Technol., Pasadena, CA, USA
fYear :
2013
fDate :
2-9 March 2013
Firstpage :
1
Lastpage :
9
Abstract :
Model-Based Systems Engineering (MBSE) is being used increasingly within the spacecraft design community because of its benefits when compared to document-based approaches. As the complexity of projects expands dramatically with continually increasing computational power and technology infusion, the time and effort needed for verification and validation (V&V) increases geometrically. Using simulation to perform design validation with system-level models earlier in the life cycle stands to bridge the gap between design of the system (based on system-level requirements) and verifying those requirements/validating the system as a whole. This case study stands as an example of how a project can validate a system-level design earlier in the project life cycle than traditional V&V processes by using simulation on a system model. Specifically, this paper describes how simulation was added to a system model of the Soil Moisture Active-Passive (SMAP) mission´s uplink process. Also discussed are the advantages and disadvantages of the methods employed and the lessons learned; which are intended to benefit future model-based and simulation-based development efforts.
Keywords :
aerospace testing; artificial satellites; remote sensing; soil; MBSE; SMAP uplink processes; design validation; model based systems engineering; model based validation; model based verification; project life cycle; soil moisture active passive mission uplink process; spacecraft design; system level design; system level model; Computational modeling; Data models; Propulsion; Space vehicles; Testing; Uplink;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2013 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4673-1812-9
Type :
conf
DOI :
10.1109/AERO.2013.6496913
Filename :
6496913
Link To Document :
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