TY - GEN
T1 - An automatic multidisciplinary design optimization framework and its application to launch vehicle
AU - Su, Hua
AU - Gong, Chunlin
AU - Gu, Liangxian
N1 - Publisher Copyright:
Copyright © 2017 by the International Astronautical Federation (IAF). All rights reserved.
PY - 2017
Y1 - 2017
N2 - Multidisciplinary Design Optimization (MDO) is the specific technique to optimize engineering problem with complex disciplines. But it's hard to select the proper MDO architecture to settle these complex problem efficiently and automatically. This paper proposed an automatic multidisciplinary design optimization framework with brief definition and clear process. Disciplinary relation matrix (DRM) is proposed to describe the coupling relationship according to disciplinary input/output variables, and the MDO definition has been reformulate to adopt the new interfaces. Based on these, a universal MDO solving procedure is proposed to establish an automated and efficient way for MDO modeling and solving. This is implemented by an object-oriented framework in C++ environment, which is called as Automatic Fast Solving Environment for MDO (AFSEMDO). And a X37B-like launch vehicle MDO problem is modeled and solved in the proposed MDO framework. Six disciplines are considered, there are geometry, aerodynamic, structure, trajectory, Mass and Control. Result shows these MDO framework can evaluate MDO problem automatically and efficiently, and could provide a more simplified way to solve complex MDO problems.
AB - Multidisciplinary Design Optimization (MDO) is the specific technique to optimize engineering problem with complex disciplines. But it's hard to select the proper MDO architecture to settle these complex problem efficiently and automatically. This paper proposed an automatic multidisciplinary design optimization framework with brief definition and clear process. Disciplinary relation matrix (DRM) is proposed to describe the coupling relationship according to disciplinary input/output variables, and the MDO definition has been reformulate to adopt the new interfaces. Based on these, a universal MDO solving procedure is proposed to establish an automated and efficient way for MDO modeling and solving. This is implemented by an object-oriented framework in C++ environment, which is called as Automatic Fast Solving Environment for MDO (AFSEMDO). And a X37B-like launch vehicle MDO problem is modeled and solved in the proposed MDO framework. Six disciplines are considered, there are geometry, aerodynamic, structure, trajectory, Mass and Control. Result shows these MDO framework can evaluate MDO problem automatically and efficiently, and could provide a more simplified way to solve complex MDO problems.
KW - MDO architecture
KW - Multidisciplinary design optimization
KW - Problem definition
KW - Solving automation
UR - http://www.scopus.com/inward/record.url?scp=85051433435&partnerID=8YFLogxK
M3 - 会议稿件
AN - SCOPUS:85051433435
SN - 9781510855373
T3 - Proceedings of the International Astronautical Congress, IAC
SP - 1399
EP - 1406
BT - 68th International Astronautical Congress, IAC 2017
PB - International Astronautical Federation, IAF
T2 - 68th International Astronautical Congress: Unlocking Imagination, Fostering Innovation and Strengthening Security, IAC 2017
Y2 - 25 September 2017 through 29 September 2017
ER -