This paper presents a new approach for optimization under uncertainty in the presence of probabilistic, interval, and mixed uncertainties, avoiding the need to specify probability distributions on uncertain parameters when such information is not readily available. Existing approaches for optimization under these types of uncertainty mostly rely on treating combinations of statistical moments as separate objectives, but this can give rise to stochastically dominated designs. Here, horsetail matching is extended for use with these types of uncertainties to overcome some of the limitations of existing approaches. The formulation delivers a single, differentiable metric as the objective function for optimization. It is demonstrated on algebrai...
Presented in this thesis is a novel methodology for aircraft design optimization in the presence of ...
The assessment of uncertainties is essential in aerodynamic shape optimization problems to come up w...
[Abstract] The subject of this paper is the conceptual design of airfoils under geometric uncertaint...
This paper presents a new approach for optimization under uncertainty in the presence of probabilist...
The importance of including uncertainties in the design process of aerospace systems is becoming inc...
The importance of including uncertainties in the design process of aerospace systems is becoming inc...
It is important to design engineering systems to be robust with respect to uncertainties in the desi...
This data comprises a python module that implements the horsetail matching method presented in this ...
The importance of designing airfoils to be robust with respect to uncertainties in operating conditi...
AbstractModern computers enable methods for design optimization that account for uncertainty in the ...
ABSTRACT: Uncertainty-based multidisciplinary design optimization considers probabilistic variables ...
Engineers agree with the fact that uncertainty is an important issue to get a better model of real b...
Modern computers enable methods for design optimization that account for uncertainty in the system -...
One of the primary objectives of this research is to develop a method to model and propagate mixed (...
The objective of this paper is to present a robust optimization algorithm for computationally effici...
Presented in this thesis is a novel methodology for aircraft design optimization in the presence of ...
The assessment of uncertainties is essential in aerodynamic shape optimization problems to come up w...
[Abstract] The subject of this paper is the conceptual design of airfoils under geometric uncertaint...
This paper presents a new approach for optimization under uncertainty in the presence of probabilist...
The importance of including uncertainties in the design process of aerospace systems is becoming inc...
The importance of including uncertainties in the design process of aerospace systems is becoming inc...
It is important to design engineering systems to be robust with respect to uncertainties in the desi...
This data comprises a python module that implements the horsetail matching method presented in this ...
The importance of designing airfoils to be robust with respect to uncertainties in operating conditi...
AbstractModern computers enable methods for design optimization that account for uncertainty in the ...
ABSTRACT: Uncertainty-based multidisciplinary design optimization considers probabilistic variables ...
Engineers agree with the fact that uncertainty is an important issue to get a better model of real b...
Modern computers enable methods for design optimization that account for uncertainty in the system -...
One of the primary objectives of this research is to develop a method to model and propagate mixed (...
The objective of this paper is to present a robust optimization algorithm for computationally effici...
Presented in this thesis is a novel methodology for aircraft design optimization in the presence of ...
The assessment of uncertainties is essential in aerodynamic shape optimization problems to come up w...
[Abstract] The subject of this paper is the conceptual design of airfoils under geometric uncertaint...