Abstract:
Most of the efforts in optimisation so far have been focused on the development of novel
or the improvement of existing numerical methods for an effective computation of
optimal solutions. Particular attention has been put on balancing multiple conflicting
objectives, handling the interaction between different disciplines, reducing computational
cost and managing uncertainty. Nonetheless, specific issues of this design methodology
still remain to be properly addressed. In this research, attention is concentrated on
advancing engineering optimisation as a tool for design exploration. The work is put in
the context of conceptual aircraft design.
The overall aim of the present research is to develop a methodology that allows the
designer to effectively conduct an exploration and analysis of alternative design solutions
via a set of methods that can be used separately or conjointly.
The initial part of the thesis introduces two novel methods for assisting the formulation of
an optimisation problem, which generally is assumed to be given a priori. Nonetheless,
the correctness of the optimisation statement, which is not addressed by established
optimisation methods, turns out to be decisive for the feasible design set determination.
The designer is thus provided with an adaptive formulation of functional and designvariable
constraints, which allows the exploration of further promising solutions initially
not contained in the feasible design set. Meaningless results or the loss of important
solutions can therefore be partially avoided.
In a second instance, attention is focused on the visualisation needs for design
exploration. A suitable visualisation methodology has been developed to make the large
multidimensional results of complex design optimisation procedures fully readable and
explanatory. This is achieved by integrating advanced visualisation techniques which provide the designer with diverse perspectives of the data under study and allow him/her
to conduct a number of analysis tasks on it, without the need to be an expert in numerical
optimisation methods.
Last, but not least, a methodology to address conceptual design change problems is
proposed. The decision-maker is enabled to formally state the new design requirements
and priorities introduced by the conceptual change via an adequate problem
reformulation. All the data previously collected can thus be re-used and exploited to drive
an effective exploration of alternative design solutions through design space regions of
interest.
The evaluation of the proposed methodologies has been carried out with a number of test
cases. Analytical examples have been used for the assessment of effectiveness, whereas
codes representative of aircraft sizing procedures have been adopted to evaluate the
methodologies functionality. A visualisation user interface prototype has also been
developed for demonstration and evaluation purposes.