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Isoperformance: Analysis and design of complex systems with desired outcomes
Author(s) -
de Weck Olivier L.,
Jones Marshall B.
Publication year - 2006
Publication title -
systems engineering
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.474
H-Index - 50
eISSN - 1520-6858
pISSN - 1098-1241
DOI - 10.1002/sys.20043
Subject(s) - maximization , computer science , set (abstract data type) , jacobian matrix and determinant , mathematical optimization , spacecraft , operations research , engineering , mathematics , programming language , aerospace engineering
The design of technical systems such as automobiles and spacecraft has traditionally focused exclusively on performance maximization. Many organizations now realize that such an approach must be balanced against competing objectives of cost, risk, and other criteria. If one is willing to give up some amount of performance relative to the best achievable performance level, one introduces slack into system design. This slack can be invested in creating better outcomes overall. One way to achieve this is to balance the requirements among contributing subsystems such that the number of active constraints is minimized, while still achieving the desired system performance. This paper introduces a methodology called “isoperformance” as a means of identifying and evaluating a performance‐invariant set of design solutions, which are efficient in terms of other criteria such as cost, risk, and lifecycle properties. Isoperformance is an inverse design method that starts from a desired vector of performance requirements and works backwards to identify acceptable solutions in the design space. To achieve this, gradient‐based contour following is implemented as a multivariable search algorithm that manipulates the null set of the Jacobian matrix. Use of the method is illustrated with two examples from spacecraft design and human performance in sports. © 2006 Wiley Periodicals, Inc. Syst Eng 9: 45–61, 2006