dc.contributor.author |
Lwin, Thandar
|
|
dc.contributor.author |
Maw, Aye Aye
|
|
dc.contributor.author |
Shu, Jung-Il
|
|
dc.contributor.author |
Kim, Jin-Wook
|
|
dc.contributor.author |
Lee, Jae-Woo
|
|
dc.contributor.author |
Kim, Sang-Ho
|
|
dc.date.accessioned |
2019-07-03T06:45:49Z |
|
dc.date.available |
2019-07-03T06:45:49Z |
|
dc.date.issued |
2016-02-25 |
|
dc.identifier.uri |
http://onlineresource.ucsy.edu.mm/handle/123456789/242 |
|
dc.description |
This work was supported by the Space
Core Technology Development Program (No.
2012033512) of the National Research
Foundation of Korea and the Ministry of
Science, ICT & Future Planning. |
en_US |
dc.description.abstract |
This study describes multidisciplinary design
framework development based on system
engineering concept for various space launch
vehicles to assist aeronautical engineers to
successfully design mission and system analysis
process. Design framework is composed of five
main stages: Requirements, Mission Analysis
and Design, System Synthesis and Simulation,
Integrated Mission Design, and Reliability and
Cost Evaluation. Two databases are established:
one is used in the process of data-mining for
requirements and another is in the Graphical
User Interface (GUI) development of framework.
K-Nearest Neighbors (k-NN) and Regression
methods are utilized to make the design
optimization performed with fast and successful
convergence by processing and estimating the
data necessary for design optimization.
Framework is mainly developed in VB.Net
integrating with all discipline modules
separately optimized in Matlab. It is
demonstrated that much better design can be
obtained by using this framework and considering the important design factors from
various disciplines. |
en_US |
dc.language.iso |
en |
en_US |
dc.publisher |
Fourteenth International Conference On Computer Applications (ICCA 2016) |
en_US |
dc.title |
Development of Mission-Design Integrated Framework for Space Launch Vehicles |
en_US |
dc.type |
Article |
en_US |