Bilevel integrated system synthesis

被引:117
作者
Sobieszczanski-Sobieski, J [1 ]
Agte, JS
Sandusky, RR
机构
[1] NASA, Langley Res Ctr, Hampton, VA 23681 USA
[2] George Washington Univ, Joint Inst Advancement Flight Sci, Washington, DC 20052 USA
关键词
D O I
10.2514/2.937
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Bilevel integrated system synthesis is a method far the optimization of engineering systems by decomposition. It separates the system level optimization, having a relatively small number of design variables, from the potentially numerous subsystem optimizations that may each have a large number of local design variables, The subsystem optimizations are autonomous and may be conducted concurrently. Subsystem and system optimizations alternate, linked by sensitivity data, producing a design improvement in each iteration, Starting from a best guess initial design, the method improves that design in iterative cycles; each cycle comprises two steps. In step one, the system level variables are frozen and the improvement is achieved by separate, concurrent, and autonomous optimizations in the local variable subdomains. In step two, further improvement is sought in the space of the system level variables. Optimum sensitivity data link the second step to the first. The method prototype was implemented using MATLAB(R) and iSIGHT programming software and tested on a simplified, conceptual level supersonic business jet design, and a detailed design of an electronic device. Satisfactory convergence and favorable agreement with the benchmark results were observed. Modularity of the method is intended to fit the human organization and map well on the computing technology of concurrent processing.
引用
收藏
页码:164 / 172
页数:9
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