DATAWorks Sessions Archive

Problems faced in defense and aerospace often go well beyond textbook problems presented in academic settings. Textbook problems are typically very well defined, and can be solved through application of one “correct” tool. Conversely, many defense and aerospace problems are ill-defined, at least initially, and require an overall strategy to attack, one involving multiple tools and often multiple disciplines. Statistical engineering is an approach recently developed for addressing large, complex, unstructured problems, particularly those for which data can be effectively utilized. This session will present a brief overview of statistical engineering, and how it can be applied to engineer solutions to complex problems. Following this introduction, two case studies of statistical engineering will be presented, to illustrate the concepts.

Problems faced in defense and aerospace often go well beyond textbook problems presented in academic settings. Textbook problems are typically very well defined, and can be solved through application of one “correct” tool. Conversely, many defense and aerospace problems are ill-defined, at least initially, and require an overall strategy to attack, one involving multiple tools and often multiple disciplines. Statistical engineering is an approach recently developed for addressing large, complex, unstructured problems, particularly those for which data can be effectively utilized. This session will present a brief overview of statistical engineering, and how it can be applied to engineer solutions to complex problems. Following this introduction, two case studies of statistical engineering will be presented, to illustrate the concepts.

Analysis-based means of compliance for airplane and engine certification, commonly known as “Certification by Analysis” (CbA), provides a strong motivation for the development and maturation of current and future flight and engine modeling technology. The most obvious benefit of CbA is streamlined product certification testing programs at lower cost while maintaining equivalent levels of safety. The current state of technologies and processes for analysis is not sufficient to adequately address most aspects of CbA today, and concerted efforts to drastically improve analysis capability are required to fully bring the benefits of CbA to fruition. While the short-term cost and schedule benefits of reduced flight and engine testing are clearly visible, the fidelity of analysis capability required to realize CbA across a much larger percentage of product certification is not yet sufficient.  Higher-fidelity analysis can help reduce the product development cycle and avoid costly and unpredictable performance and operability surprises that sometimes happen late in the development cycle. Perhaps the greatest long-term value afforded by CbA is the potential to accelerate the introduction of more aerodynamically and environmentally efficient products to market, benefitting not just manufacturers, but also airlines, passengers, and the environment. A far-reaching vision for CbA has been constructed to offer guidance in developing lofty yet realizable expectations regarding technology development and maturity through stakeholder involvement. This vision is composed of the following four elements: The ability to numerically simulate the integrated system performance and response of full-scale airplane and engine configurations in an accurate, robust, and computationally efficient manner. The development of quantified flight and engine modeling uncertainties to establish appropriate confidence in the use of numerical analysis for certification. The rigorous validation of flight and engine modeling capabilities against full-scale data from critical airplane and engine testing. The use of flight and engine modeling to enable Certification by Simulation. Key technical challenges include the ability to accurately predict airplane and engine performance for a single discipline, the robust and efficient integration of multiple disciplines, and the appropriate modeling of system-level assessment. Current modeling methods lack the capability to adequately model conditions that exist at the edges of the operating envelope where the majority of certification testing generally takes place.  Additionally, large-scale engine or airplane multidisciplinary integration has not matured to the level where it can be reliably used to efficiently model the intricate interactions that exist in current or future aerospace products. Logistical concerns center primarily on the future High Performance Computing capability needed to perform the large number of computationally intensive simulations needed for CbA. Complex, time-dependent, multidisciplinary analyses will require a computing capacity increase several orders of magnitude greater than is currently available. Developing methods to ensure credible simulation results is critically important for regulatory acceptance of CbA. Confidence in analysis methodology and solutions is examined so that application validation cases can be properly identified. Other means of measuring confidence such as uncertainty quantification and “validation-domain” approaches may increase the credibility and trust in the predictions. Certification by Analysis is a challenging long-term endeavor that will motivate many areas of simulation technology development, while driving the potential to decrease cost, improve safety, and improve airplane and engine efficiency. Requirements to satisfy certification regulations provide a measurable definition for the types of analytical capabilities required for success. There is general optimism that CbA is a goal that can be achieved, and that a significant amount of flight testing can be reduced in the next few decades.

Equipment Failure Reports (EFRs) describe equipment failures and the steps taken as a result of these failures. EFRs contain both structured and unstructured data. Currently, analysts manually read through EFRs to understand failure modes and make recommendations to reduce future failures. This is a tedious process where important trends and information can get lost. This motivated the creation of an interactive dashboard that extracts relevant information from the unstructured (i.e. free-form text) data and combines it with structured data like failure date, corrective action and part number. The dashboard is an RShiny application that utilizes numerous text mining and visualization packages, including tm, plotly, edgebundler, and topicmodels. It allows the end-user to filter to the EFRs that they care about and visualize meta-data, such as geographic region where the failure occurred, over time allowing previously unknown trends to be seen. The dashboard also applies topic modeling to the unstructured data to identify key themes. Analysts are now able to quickly identify frequent failure modes and look at time and region-based trends in these common equipment failures.

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.

Cybersecurity Metrics and Quantification is a fundamental but notoriously hard problem. It is one of the pillars underlying the emerging Science of Cybersecurity. In this talk, I will describe a number of cybersecurity metrics quantification research problems that are encountered in evaluating the effectiveness of a range of cyber defense tools. I will review the research results we have obtained over the past years. I will also discuss future research directions, including the ones that are undertaken in my research group.

Development of new technology always incorporates model testing. This is certainly true for hypersonics, where flight tests are expensive and testing of component- and system-level models has significantly advanced the field. Unfortunately, model tests are often limited in scope, being only approximations of reality and typically only partially covering the range of potential realistic conditions. In this talk, we focus on the problem of real-time detection of the shock train leading edge in high-speed air-breathing engines, such as dual-mode scramjets. Detecting and controlling the shock train leading edge is important to the performance and stability of such engines, and a problem that has seen significant model testing on the ground and some flight testing. Often, methods developed for shock train detection are specific to the model used. Thus, they may not generalize well when tested in another facility or in flight as they typically require a significant amount of prior characterization of the model and flow regime. A successful method for shock train detection needs to be robust to changes in features like isolator geometry, inlet and combustor states, flow regimes, and available sensors. Such data can be difficult or impossible to obtain if the isolator operating regime is large. To this end, we propose the an approach for real-time detection of the isolator shock train. Our approach uses real-time pressure measurements to adaptively estimate the shock train position in a data-driven manner. We show that the method works well across different isolator models, placement of pressure transducers, and flow regimes. We believe that a data-driven approach is the way forward for bridging the gap between testing and reality, saving development time and money.

In design of experiments, setting exact replicates of factor settings enables estimation of pure-error; a model-independent estimate of experimental error useful in communicating inherent system noise and testing of model lack-of-fit. Often in practice, the factor levels for replicates are precisely measured rather than precisely set, resulting in near-replicates. This can result in inflated estimates of pure-error due to uncompensated set-point variation. In this article, we review previous strategies for estimating pure-error from near-replicates and propose a simple alternative. We derive key analytical properties and investigate them via simulation. Finally, we illustrate the new approach with an application.

The Advanced Joint Effectiveness Model (AJEM) is a joint forces model developed by the U.S. Army that is used in vulnerability and lethality (V/L) predictions for threat/target interactions. This complex model primarily generates a probability response for various components, scenarios, loss of capabilities, or summary conditions. Sensitivity analysis (SA) and uncertainty quantification (UQ), referred to jointly as SA/UQ, are disciplines that provide the working space for how model estimates changes with respect to changes in input variables. A comparative measure that will be used to characterize the effect of an input change on the predicted outcome was developed and is reviewed and illustrated in this presentation. This measure provides a practical context that stakeholders can better understand and utilize. We show graphical and tabular results using this measure.

Generating aerodynamic coefficients can be computationally expensive, especially for the viscous CFD solvers in which multiple complex models are iteratively solved. When filling large design spaces, utilizing only a high accuracy viscous CFD solver can be infeasible. We apply state-of-the-art methods for design and analysis of computer experiments to efficiently develop an emulator for high-fidelity simulations. First, we apply a cokriging model to leverage information from fast low-fidelity simulations to improve predictions with more expensive high-fidelity simulations. Combining space-filling designs with a Gaussian process model-based sequential sampling criterion allows us to efficiently generate sample points and limit the number of costly simulations needed to achieve the desired model accuracy. We demonstrate the effectiveness of these methods with an aerodynamic simulation study using a conic shape geometry. This work was performed under the auspices of the U.S. Department of Energy by Lawrence Livermore National Laboratory under Contract DE-AC52-07NA27344. Release Number: LLNL-ABS-818163