Autonomous experimental design optimization

Abstract

Iterative (nondeterministic) optimization of aerodynamic and hydrodynamic surface structures can be accomplished with a computer software program and a system using a combination of a variable encoding length optimization algorithm based on an evolution strategy and an experimental hardware set-up that allows to automatically change the surface properties of the applied material, starting with the overall shape and proceeding via more detailed modifications in local surface areas. The optimization of surface structures may be done with a computing device for calculating optimized parameters of at least one (virtual) surface structure, an experimental hardware set-up for measuring dynamic properties of a specific surface structure, and an interface for feeding calculated parameters from the computing device to the experimental set-up and for feeding measured results back to the computing device as quality values for the next cycle of the optimizing step.

Description

RELATED FOREIGN APPLICATIONS[0001]This application is related and claims priority to European Patent Application No. 02 013 826.9 filed on Jun. 21, 2002 by Bernhard Sendhoff, Edgar Korner, and Andreas Richter, titled “Autonomous Experimental Design Optimization”.FIELD OF THE INVENTION[0002]The underlying invention generally relates to the optimization of aerodynamic and hydrodynamic designs, in particular to methods for an iterative (non-deterministic) optimization of hydrodynamic and aerodynamic surfaces, e.g., aircrafts, ships and vehicles, a computer software program for implementing such a method as well as to systems for optimizing said surfaces.BACKGROUND OF THE INVENTION[0003]Some aspects of the invention involve the advantageous use of technologies known in the art. In the following description some of these basic technologies will be introduced, for example, CFD, Gradient based methods, Evolutionary Algorithms (EA), and Artificial 25 Neuronal Networks (ANN).[0004]Computatio...

AI Technical Summary

Problems solved by technology

However, CFD simulations are computationally very expensive.

What makes the problem more difficult is that EAs need a relatively large number of evaluations in order to achieve a near optimal aerodynamic design.

An important issue that is closely related to ANNs is learning.

Consequently, this approach has been widely used for many design problems including wing design, nozzle design, supersonic wing-body design, and more complex aircraft configurations.

The quality landscape for an aerodynamic design problem, however, is usually multimodal.

In this sense, GMs are neither efficient nor robust for design optimization.

This process can be computationally expensive and in general it is not very robust against noise.

However, Otto et al. do not disclose the use of EAs for said optimization process.

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