The design process of FCG configuration involves mathematical modeling of the geometry and parametric evaluation of various independent geometric variables that define the complex configuration.
Accordingly, this paper proposes a hybrid framework that combines fuzzy analytical hierarchy process (AHP), fuzzy Kano model with zero-one integer programming (ZOIP) to incorporate customer preferences and customer perceptions into the decision-making process of product configuration.
The proposed methodology is illustrated and validated in the process of designing configurations for automotive underbody subassembly.
The chapter illustrates in detail the processes of installation, configuration, testing the database, database design, and issues with it.
The paper by Cook et al. highlights the importance of manageability in cloud environments, where manageability is defined as "the collective processes of deployment, configuration, optimisation, and administration during the lifecycle of IT systems and services".
A simultaneous optimization framework is presented that addresses the problem of optimal allocation of reliability among equipment simultaneously with the selection of process configuration, production and maintenance planning for multipurpose process plants at the design stage.
At first sight it might seem rather extensive, but the applied color coding eases the process of grasping the configuration details.
In the process of the optimisation, configuration of the elastic materials is expressed with a level set function, and the distribution of the level set function is iteratively updated with the help of the topological derivative.
Also the necessity to obtain a surround of automatic systems development which integrates all the necessary elements in order to automate the whole process of development, debugging, configuration and verification is discussed.
Thus, taking into account the coupling and interference factors, the multidimensional gaming model based on aircraft components will be an effective analysis method in the decision-making process of aircraft optimum configuration.
