Brian Milne Rutherford
Sandia National Laboratories
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Featured researches published by Brian Milne Rutherford.
Reliability Engineering & System Safety | 2002
William L. Oberkampf; Sharon M. DeLand; Brian Milne Rutherford; Kathleen V. Diegert; Kenneth F. Alvin
Abstract This article develops a general framework for identifying error and uncertainty in computational simulations that deal with the numerical solution of a set of partial differential equations (PDEs). A comprehensive, new view of the general phases of modeling and simulation is proposed, consisting of the following phases: conceptual modeling of the physical system, mathematical modeling of the conceptual model, discretization and algorithm selection for the mathematical model, computer programming of the discrete model, numerical solution of the computer program model, and representation of the numerical solution. Our view incorporates the modeling and simulation phases that are recognized in the systems engineering and operations research communities, but it adds phases that are specific to the numerical solution of PDEs. In each of these phases, general sources of uncertainty, both aleatory and epistemic, and error are identified. Our general framework is applicable to any numerical discretization procedure for solving ODEs or PDEs. To demonstrate this framework, we describe a system-level example: the flight of an unguided, rocket-boosted, aircraft-launched missile. This example is discussed in detail at each of the six phases of modeling and simulation. Two alternative models of the flight dynamics are considered, along with aleatory uncertainty of the initial mass of the missile and epistemic uncertainty in the thrust of the rocket motor. We also investigate the interaction of modeling uncertainties and numerical integration error in the solution of the ordinary differential equations for the flight dynamics.
Other Information: PBD: 1 Mar 2000 | 2000
Kenneth F. Alvin; William L. Oberkampf; Brian Milne Rutherford; Kathleen V. Diegert
This research effort focuses on methodology for quantifying the effects of model uncertainty and discretization error on computational modeling and simulation. The work is directed towards developing methodologies which treat model form assumptions within an overall framework for uncertainty quantification, for the purpose of developing estimates of total prediction uncertainty. The present effort consists of work in three areas: framework development for sources of uncertainty and error in the modeling and simulation process which impact model structure; model uncertainty assessment and propagation through Bayesian inference methods; and discretization error estimation within the context of non-deterministic analysis.
Reliability Engineering & System Safety | 2006
Brian Milne Rutherford
Abstract Often, the objectives in a computational analysis involve characterization of system performance based on some function of the computed response. In general, this characterization includes (at least) an estimate or prediction for some performance measure and an estimate of the associated uncertainty. Surrogate models can be used to approximate the response in regions where simulations were not performed. For most surrogate modeling approaches, however, (1) estimates are based on smoothing of available data and (2) uncertainty in the response is specified in a point-wise (in the input space) fashion. These aspects of the surrogate model construction might limit their capabilities. One alternative is to construct a probability measure, G(r), for the computer response, r, based on available data. This “response-modeling” approach will permit probability estimation for an arbitrary event, E(r), based on the computer response. In this general setting, event probabilities can be computed: prob(E)=∫rI(E(r))dG(r) where I is the indicator function. Furthermore, one can use G(r) to calculate an induced distribution on a performance measure, pm. For prediction problems where the performance measure is a scalar, its distribution Fpm is determined by: Fpm(z)=∫rI(pm(r)⩽z)dG(r). We introduce response models for scalar computer output and then generalize the approach to more complicated responses that utilize multiple response models.
Reliability Engineering & System Safety | 2004
Brian Milne Rutherford
Abstract Computational simulation methods have advanced to a point where simulation can contribute substantially in many areas of systems analysis. One research challenge that has accompanied this transition involves the characterization of uncertainty in both computer model inputs and the resulting system response. This article addresses a subset of the ‘challenge problems’ posed in [Challenge problems: uncertainty in system response given uncertain parameters, 2001] where uncertainty or information is specified over intervals of the input parameters and inferences based on the response are required. The emphasis of the article is to describe and illustrate a method for performing tasks associated with this type of modeling ‘economically’-requiring relatively few evaluations of the system to get a precise estimate of the response. This ‘response-modeling approach’ is used to approximate a probability distribution for the system response. The distribution is then used: (1) to make inferences concerning probabilities associated with response intervals and (2) to guide in determining further, informative, system evaluations to perform.
Archive | 2000
William L. Oberkampf; Sharon M. DeLand; Brian Milne Rutherford; Kathleen V. Diegert; D. F. Alvin
Archive | 1998
William L. Oberkampf; Kathleen V. Diegert; Kenneth F. Alvin; Brian Milne Rutherford
Computer Methods in Applied Mechanics and Engineering | 2008
Brian Milne Rutherford
Computer Methods in Applied Mechanics and Engineering | 2008
Brian Milne Rutherford
Optimization and Engineering | 2006
Brian Milne Rutherford
Archive | 2012
Rene L. Bierbaum; Justin T. Newcomer; Edward Victor Thomas; Brian Milne Rutherford; Kathleen V. Diegert; Joseph D. Warfield