DATAWorks Sessions Archive

Rigorous characterization of system capabilities is essential for defensible decisions in test and evaluation (T&E). Analysis of designed experiments is not usually associated “big” data analytics as there are typically a modest number of runs, factors, and responses. The Mars Rover program has recently conducted several disciplined DOEs on prototype coring drill performance with approximately 10 factors along with scores of responses and hundreds of recorded covariates. The goal is to characterize the ‘atthis-time’ capability to confirm what the scientists and engineers already know about the system, answer specific performance and quality questions across multiple environments, and inform future tests to optimize performance. A ‘rigorous’ characterization required that not just one analytical path should be taken, but a combination of interactive data visualization, classic DOE analysis screening methods, and newer methods from predictive analytics such as decision trees. With hundreds of response surface models across many test series and qualitative factors, these methods used had to efficiently find the signals hidden in the noise. Participants will be guided through an end-to-end analysis workflow with actual data from many tests (often Definitive Screening Designs) of the Rover prototype coring drill. We will show data assembly, data cleaning (e.g. missing values and outliers), data exploration with interactive graphical designs, variable screening, response partitioning, data tabulation, model building with stepwise and other methods, and model diagnostics. Software packages such as R and JMP will be used.

Rigorous characterization of system capabilities is essential for defensible decisions in test and evaluation (T&E). Analysis of designed experiments is not usually associated “big” data analytics as there are typically a modest number of runs, factors, and responses. The Mars Rover program has recently conducted several disciplined DOEs on prototype coring drill performance with approximately 10 factors along with scores of responses and hundreds of recorded covariates. The goal is to characterize the ‘atthis-time’ capability to confirm what the scientists and engineers already know about the system, answer specific performance and quality questions across multiple environments, and inform future tests to optimize performance. A ‘rigorous’ characterization required that not just one analytical path should be taken, but a combination of interactive data visualization, classic DOE analysis screening methods, and newer methods from predictive analytics such as decision trees. With hundreds of response surface models across many test series and qualitative factors, these methods used had to efficiently find the signals hidden in the noise. Participants will be guided through an end-to-end analysis workflow with actual data from many tests (often Definitive Screening Designs) of the Rover prototype coring drill. We will show data assembly, data cleaning (e.g. missing values and outliers), data exploration with interactive graphical designs, variable screening, response partitioning, data tabulation, model building with stepwise and other methods, and model diagnostics. Software packages such as R and JMP will be used.

Is there ever a place for the third dimension in visualizing data? Is the use of 3D inherently bad, or can a 3D visualization be used as an effective tool to communicate results? In this talk, I will show you how you can create beautiful 2D and 3D maps and visualizations in R using the rayshader package. Additionally, I will talk about the value of 3D plotting and how good aesthetic choices can more clearly communicate results to stakeholders. Rayshader is a free and open source package for transforming geospatial data into engaging visualizations using a simple, scriptable workflow. It provides utilities to interactively map, plot, and 3D print data from within R. It was nominated by Hadley Wickham to be one of 2018’s Data Visualizations of the Year for the online magazine Quartz.

Computational fluid dynamics is now considered to be an indispensable tool for the design and development of scramjet engine components. Unfortunately, the quantification of uncertainties is rarely addressed with anything other than sensitivity studies, so the degree of confidence associated with the numerical results remains exclusively with the subject matter expert that generated them. This practice must be replaced with a formal uncertainty quantification process for computational fluid dynamics to play an expanded role in the system design, development, and flight certification process. Given the limitations of current hypersonic ground test facilities, this expanded role is believed to be a requirement by some in the hypersonics community if scramjet engines are to be given serious consideration as a viable propulsion system. The present effort describes a simple, relatively low cost, nonintrusive approach to uncertainty quantification that includes the basic ingredients required to handle both aleatoric (random) and epistemic (lack of knowledge) sources of uncertainty. The nonintrusive nature of the approach allows the computational fluid dynamicist to perform the uncertainty quantification with the flow solver treated as a “black box”. Moreover, a large fraction of the process can be automated, allowing the uncertainty assessment to be readily adapted into the engineering design and development workflow. In the present work, the approach is applied to a model scramjet isolator problem where the desire is to validate turbulence closure models in the presence of uncertainty. In this context, the relevant uncertainty sources are determined and accounted for to allow the analyst to delineate turbulence model-form errors from other sources of uncertainty associated with the simulation of the facility flow.

Causality in an engineered system pertains to how a system output changes due to a controlled change or intervention on the system or system environment. Engineered systems designs reflect a causal theory regarding how a system will work, and predicting the reliability of such systems typically requires knowledge of this underlying causal structure. The aim of this work is to introduce causal modeling tools that inform reliability predictions based on biased data sources and illustrate how these tools can inform data integration in practice. We present a novel application of the popular structural causal modeling framework to reliability estimation in an engineering application, illustrating how this framework can inform whether reliability is estimable and how to estimate reliability using data integration given a set of assumptions about the subject matter and data generating mechanism. When data are insufficient for estimation, sensitivity studies based on problem-specific knowledge can inform how much reliability estimates can change due to biases in the data and what information should be collected next to provide the most additional information. We apply the approach to a pedagogical example related to a real, but proprietary, engineering application, considering how two types of biases in data can influence a reliability calculation.

This session will focus on the novel application of a design of experiments approach to optimize a propulsion charge configuration for a U.S. Army artillery round. The interdisciplinary design effort included contributions from subject matter experts in statistics, propulsion charge design, computational physics and experimentation. The process, which we will present in this session, consisted of an initial, low fidelity modeling and simulation study to reduce the parametric space by eliminating inactive variables and reducing the ranges of active variables for the final design. The final design used a multi-tiered approach that consolidated data from multiple sources including low fidelity modeling and simulation, high fidelity modeling and simulation and live test data from firings in a ballistic simulator. Specific challenges of the effort that will be addressed include: integrating data from multiple sources, a highly constrained design space, functional response data, multiple competing design objectives and real-world test constraints. The result of the effort is a final, optimized propulsion charge design that will be fabricated for live gun firing.

This session will focus on the novel application of a design of experiments approach to optimize a propulsion charge configuration for a U.S. Army artillery round. The interdisciplinary design effort included contributions from subject matter experts in statistics, propulsion charge design, computational physics, and experimentation. The process, which we will present in this session, consisted of an initial, low fidelity modeling and simulation study to reduce the parametric space by eliminating inactive variables and reducing the ranges of active variables for the final design. The final design used a multi-tiered approach that consolidated data from multiple sources including low fidelity modeling and simulation, high fidelity modeling and simulation and live test data from firings in a ballistic simulator. Specific challenges of the effort that will be addressed include: integrating data from multiple sources, a highly constrained design space, functional response data, multiple competing design objectives, and real-world test constraints. The result of the effort is a final, optimized propulsion charge design that will be fabricated for live gun firing.

When developing a system, it is important to consider system performance from a user perspective. This can be done through operational testing—assessing the ability of representative users to satisfactorily accomplish tasks or missions with the system in operationally-representative environments. This process can be expensive and time-consuming, but is critical for evaluating a system. We show how an existing design of experiments (DOE) process for operational testing can be leveraged to construct a Bayesian adaptive design. This method, nested within the larger design created by the DOE process, allows interim analyses using predictive probabilities to stop testing early for success or futility. Furthermore, operational environments with varying probabilities of encountering are directly used in product evaluation. Representative simulations demonstrate how these interim analyses can be used in an operational test setting, and reductions in necessary test events are shown. The method allows for using either weakly informative priors when data from previous testing is not available, or for priors built using developmental testing data when it is available. The proposed method for creating priors using developmental testing data allows for more flexibility in which data can be incorporated into analysis than the current process does, and demonstrates that it is possible to get more precise parameter estimates. This method will allow future testing to be conducted in less time and at less expense, on average, without compromising the ability of the existing process to verify the system meets the user’s needs.

The Scientific Test and Analysis Techniques (STAT) process is designed to provide structure for a test team to progress from a requirement to decision quality information. The four phases of the STAT process are Plan, Design, Execute, and Analyze. Within the Test and Evaluation (T&E) community we tend to focus on the quantifiable metrics and the hard science of testing, which are the Design and the Analyze phases. At the STAT Center of Excellence (COE) we have emphasized an increased focus on the planning phase and in this presentation we focus on the elements necessary for a comprehensive planning session. In order to efficiently and effectively test a system it is vital that the test team understand the requirements, the System Under Test (SUT) to include any subsystems that will be tested, and the test facility. To accomplish this the right team members with the necessary knowledge must be in the room and prepared to present their information and have an educated discussion to arrive at a comprehensive agreement about the desired end stated of the test. Our recommendations for the initial planning meeting are based on a thorough study of the STAT process and on lessons learned from actual planning meetings.

Humans are not produced in quality-controlled assembly lines, and we typically are much more variable than the mechanical systems we employ. This mismatch means that when characterizing the effectiveness of a system, the system must be considered in the context of its users. Accurate measurement is critical to this endeavor, yet while human variability is large, effort to reduce measurement error of those humans is relatively small. The following talk discusses the importance of using multiple measurement methods—triangulation—to reduce error and increase confidence when characterizing the quality of HSI. A case study from an operational test of an attack helicopter demonstrates how triangulation enables more actionable recommendations.

Existing characterization of Europa’s environment is enabled by the Europa Clipper mission’s successful predecessors: Pioneer, Voyager, Galileo, and most recently, Juno. These missions reveal high intensity energetic particle fluxes at Europa’s orbit, requiring a multidimensional design challenge to ensure mission success (i.e. meeting Level 1 science requirements). Risk averse JPL Design Principles and the Europa Environment Requirement Document (ERD) dictate practices and policy, which if masterfully followed, are designed to protect Clipper from failure or degradation due to radiation. However, even if workmanship is flawless and no waivers are assessed, modeling errors, shielding uncertainty, and natural variation in the Europa environment are cause for residual concern. While failure and part degradation are of paramount concern, the occurrence of temporary outages, causing loss or degradation of science observations, is also a critical mission risk, left largely unmanaged by documents like the ERD. The referenced risk is monitored and assessed through a Project Systems Engineering-led mission robustness effort, which attempts balance the risk of science data loss with potential design cost and increased mission complexity required to mitigate such risk. The Science Sensitivity Model (SSM) was developed to assess mission and science robustness, with its primary goal being to ensure a high probability of achieving Level 1 (L1) science objectives by informing the design of a robust spacecraft, instruments, and mission design. This discussion will provide an overview of the problem, the model, and solution strategies. Subsequent presentations discuss the experimental design used to understand the problem space and the graphics and visualization used to reveal important conclusions.

Uncertainty quantification (UQ) has emerged as the science of quantitative characterization and reduction of uncertainties in simulation and testing. Stretching across applied mathematics, statistics, and engineering, UQ is a multidisciplinary field with broad applications. A popular UQ method to analyze the effects of input variability and uncertainty on the system responses is generalized Polynomial Chaos Expansion (gPCE). This method was developed using applied mathematics and does not require knowledge of a simulation’s physics. Thus, gPCE may be used across disparate industries and is applicable to both individual component and system level simulations. The gPCE method can encounter problems when any of the input configurations fail to produce valid simulation results. gPCE requires that results be collected on a sparse grid Design of Experiment (DOE), which is generated based on probability distributions of the input variables. A failure to run the simulation at any one input configuration can result in a large decrease in the accuracy of a gPCE. In practice, simulation data sets with missing values are common because simulations regularly yield invalid results due to physical restrictions or numerical instability. We propose a statistical approach to mitigating the cost of missing values. This approach yields accurate UQ results if simulation failure makes gPCE methods unreliable. The proposed approach addresses this missing data problem by introducing an iterative machine learning algorithm. This methodology allows gPCE modelling to handle missing values in the sparse grid DOE. The study will demonstrate the convergence characteristics of the methodology to reach steady state values for the missing points using a series of simulations and numerical results. Remarks about the convergence rate and the advantages and feasibility of the proposed methodology will be provided. Several examples are used to demonstrate the proposed framework and its utility including a secondary air system example from the jet engine industry and several non-linear test functions. This is based on joint work with Dr. Mark Andrews at SmartUQ.

This case study highlights activities performed during the front-end process of a software development effort undertaken by the Fire Support Command and Control Program Office. This program office provides the U.S. Army, Joint and coalition commanders with the capability to plan, execute and deliver both lethal and non-lethal fires. Recently, the program office has undertaken modernization of its primary field artillery command and control system that has been in use for over 30 years. The focus of this case study is on the user-centered design process and activities taken prior to and immediately following contract award. A modified waterfall model comprised of three cyclic, yet overlapping phases (observation, visualization, and evaluation) provided structure for the iterative, user-centered design process. Gathering and analyzing data collected during focus groups, observational studies, and workflow process mapping, enabled the design team to identify 1) design patterns across the role/duty, unit and echelon matrix (a hierarchical organization structure), 2) opportunities to automate manual processes, 3) opportunities to increase efficiencies for fire mission processing, 4) bottlenecks and workarounds to be eliminated through design of the modernized system, 5) shortcuts that can be leveraged in design, 6) relevant and irrelevant content for each user population for streamlining access to functionality, 7) a usability baseline for later comparison (e.g., the number of steps and time taken to perform a task as captured in workflows for comparison to the same task in the modernized system), and provided the basis for creating visualizations using wireframes. Heuristic evaluations were conducted early to obtain initial feedback from users. In the next few months, usability studies will enable users to provide feedback based on actual interaction with the newly designed software. Included in this case study are descriptions of the methods used to collect user-centered design data, how results were visualized/documented for use by the development team, and lessons learned from applying user-centered design techniques during software development of a military field artillery command and control system.

Scientific computing has undergone extraordinary growth in sophistication in recent years, enabling the simulation of a wide range of complex multiphysics and multiscale phenomena. Along with this increase in computational capability is the growing recognition that uncertainty quantification (UQ) must go hand-in-hand with numerical simulation in order to generate meaningful and reliable predictions for engineering applications. If not rigorously considered, uncertainties due to manufacturing defects, material variability, modeling assumptions, etc. can cause a substantial disconnect between simulation and reality. Packaging these complex computational models within an UQ framework, however, can be a significant challenge due to the need to repeatedly evaluate the model when even a single evaluation is time-consuming. This talk discusses efforts at NASA Langley Research Center (LaRC) to enable rapid UQ for problems with expensive computational models. Under the High Performance Computing Incubator (HPCI) program at LaRC, several open-source software libraries are being developed and released to provide access to general-purpose, state-of-the-art UQ algorithms. The common denominator of these methods is that they all expose parallelism among the model evaluations needed for UQ and, as such, are implemented to leverage HPC resources when available to achieve tremendous computational speedup. While the methods and software presented are broadly applicable, they will be demonstrated in the context of applications that have particular interest at NASA, including structural health management and trajectory simulation.

The American National Standards Institute (ANSI) maintains a set of test standards that provide methods to characterize and determine the acceptability of radiation detection systems for use in Homeland security. With a focus on the environmental, electromagnetic, and mechanical functionality tests, we describe the test formulation and discuss challenges faced in administering the standard to include the assurance of comparable evaluations across multiple test facilities and the handling of systems that provide a non-standard, unit-less response. We present proposed solutions to these difficulties that are currently being considered in updated versions of the ANSI standards. We briefly describe a decision analytic approach that could allow for the removal of minimum performance requirements from the standards and enable the end user to determine system suitability based on operation-specific requirements.

During the past several years, the DoD has begun applying rapid prototyping and fielding authorities—granted by Congress in the FY2016-FY2018 National Defense Authorization Acts (NDAA)—to many acquisition programs. Other programs have implemented an agile acquisition strategy where incremental capability is delivered in iterative cycles. As a result, Operational Test Agencies (OTA) have had to adjust their test processes to accommodate shorter test timelines and periodic delivery of capability to the warfighter. In this session, representatives from the Service OTAs will brief examples where they have implemented new practices and processes for conducting Operational Test on acquisition programs categorized as agile, DevOps, and/or Section 804 rapid-acquisition efforts. During the final 30 minutes of the session, a panel of OTA representatives will field questions from the audience concerning the challenges and opportunities related to test design, data collection, and analysis, that rapid-acquisition programs present.

Using Combinatorial Test Design methods to select software test scenarios has repeatedly delivered large efficiency and thoroughness gains – which begs the questions: • Why are these proven methods not used everywhere? • Why do some efforts to promote adoption of new approaches stagnate? • What steps can leaders take to introduce successfully introduce and spread new test design methods? For more than a decade, Justin Hunter has helped large global organizations across six continents adopt new test design techniques at scale. Working in some environments, he has felt like Sisyphus, forever condemned to roll a boulder uphill only to watch it roll back down again. In other situations, things clicked; teams smoothly adopted new tools and techniques, and impressive results were quickly achieved. In this presentation, Justin will discuss several common challenges faced by large organizations, explain why adopting test design tools is more challenging than adopting other types of development and testing tools, and share actionable recommendations to consider when you roll out new test design approaches.