Collaborative optimization (CO) is a multidisciplinary design optimization (MDO) method with bilevel computational structure, which decomposes the original optimization problem into one system-level problem and several subsystem problems. The strategy of decomposition in CO is a useful way for solving large engineering design problems. However, the computational difficulties caused by the system-level consistency equality constraints hinder the development of CO. In this paper, an alternative formulation of CO called CO with combination of linear approximations (CLA-CO) is presented based on the geometric analysis of CO, which is more intuitive and direct than the previous algebraic analysis. In CLA-CO, the consistency equality constraints in CO are replaced by linear approximations to the subsystem responses. As the iterative process goes on, more linear approximations are added into the system level. Consequently, the combination of these linear approximations makes the system-level problem gradually approximate the original problem. In CLA-CO, the advantages of the decomposition strategy are maintained while the computational difficulties of the conventional CO are avoided. However, there are still difficulties in applying the presented CLA-CO to problems with nonconvex constraints. The application of CLA-CO to three optimization problems, a numerical test problem, a composite beam design problem, and a gear reducer design problem, illustrates the capabilities and limitations of CLA-CO.
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An Alternative Formulation of Collaborative Optimization Based on Geometric Analysis
Xiang Li,
Xiang Li
School of Aerospace Engineering,Beijing Institute of Technology, Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education
, Beijing 100081, China
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Changan Liu,
Changan Liu
Xi’an Aerospace Propulsion Institute
, Xi’an 710100, China
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Weiji Li,
Weiji Li
School of Aeronautics, Northwestern Polytechnical University
, Xi’an 710072, China
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Teng Long
Teng Long
School of Aerospace Engineering, Beijing Institute of Technology, Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education
, Beijing 100081, China
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Xiang Li
School of Aerospace Engineering,Beijing Institute of Technology, Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education
, Beijing 100081, China
e-mail:
Changan Liu
Xi’an Aerospace Propulsion Institute
, Xi’an 710100, China
e-mail:
Weiji Li
School of Aeronautics, Northwestern Polytechnical University
, Xi’an 710072, China
e-mail:
Teng Long
School of Aerospace Engineering, Beijing Institute of Technology, Key Laboratory of Dynamics and Control of Flight Vehicle, Ministry of Education
, Beijing 100081, China
e-mail: J. Mech. Des. May 2011, 133(5): 051005 (11 pages)
Published Online: June 6, 2011
Article history
Received:
September 8, 2010
Revised:
March 30, 2011
Online:
June 6, 2011
Published:
June 6, 2011
Citation
Li, X., Liu, C., Li, W., and Long, T. (June 6, 2011). "An Alternative Formulation of Collaborative Optimization Based on Geometric Analysis." ASME. J. Mech. Des. May 2011; 133(5): 051005. https://doi.org/10.1115/1.4003919
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