A nudged hybrid analysis and modeling approach for realtime wake-vortex transport and decay prediction

被引:6
|
作者
Ahmed, Shady E. [1 ]
Pawar, Suraj [1 ]
San, Omer [1 ]
Rasheed, Adil [2 ]
Tabib, Mandar [3 ]
机构
[1] Oklahoma State Univ, Sch Mech & Aerosp Engn, Stillwater, OK 74078 USA
[2] Norwegian Univ Sci & Technol, Dept Engn Cybernet, N-7465 Trondheim, Norway
[3] SINTEF Digital, Math & Cybernet, CSE Grp, N-7034 Trondheim, Norway
关键词
Wake vortex; Digital twins; Nudging; Data fusion; Nonlinear filtering; Galerkin projection; Model order reduction; Proper orthogonal decomposition; Sparse reconstruction; Closure modeling;
D O I
10.1016/j.compfluid.2021.104895
中图分类号
TP39 [计算机的应用];
学科分类号
081203 ; 0835 ;
摘要
We put forth a long short-term memory (LSTM) nudging framework for the enhancement of reduced order models (ROMs) of fluid flows utilizing noisy measurements for air traffic improvements. Toward emerging applications of digital twins in aviation, the proposed approach allows for constructing a realtime predictive tool for wake-vortex transport and decay systems. We build on the fact that in realistic application, there are uncertainties in initial and boundary conditions, model parameters, as well as measurements. Moreover, conventional nonlinear ROMs based on Galerkin projection (GROMs) suffer from imperfection and solution instabilities, especially for advection-dominated flows with slow decay in the Kolmogorov n-width. In the presented LSTM nudging (LSTM-N) approach, we fuse forecasts from a combination of imperfect GROM and uncertain state estimates, with sparse Eulerian sensor measurements to provide more reliable predictions in a dynamical data assimilation framework. We illustrate our concept by solving the two-dimensional vorticity transport equation. We investigate the effects of measurements noise and state estimate uncertainty on the performance of the LSTM-N behavior. We also demonstrate that it can sufficiently handle different levels of temporal and spatial measurement sparsity, and offer a huge potential in developing next-generation digital twin technologies for aerospace applications. (C) 2021 Elsevier Ltd. All rights reserved.
引用
收藏
页数:14
相关论文
共 50 条
  • [1] Multimodel Ensemble Methods for Prediction of Wake-Vortex Transport and Decay
    Koerner, Stephan
    Ahmad, Nash'at N.
    Holzaepfel, Frank
    VanValkenburg, Randal L.
    [J]. JOURNAL OF AIRCRAFT, 2017, 54 (05): : 1849 - 1859
  • [2] Wake-Vortex Decay in External Turbulence
    Geurts, Bernard J.
    Kuczaj, Arkadiusz K.
    [J]. DIRECT AND LARGE-EDDY SIMULATION VII, 2010, 13 : 513 - +
  • [3] Reduction of uncertainties in prediction of wake-vortex locations
    Rossow, Vernon J.
    [J]. Journal of Aircraft, 1600, 39 (04): : 587 - 596
  • [4] Reduction of uncertainties in prediction of wake-vortex locations
    Rossow, VJ
    [J]. JOURNAL OF AIRCRAFT, 2002, 39 (04): : 587 - 596
  • [5] Aircraft Wake-Vortex Encounter Analysis for Upper Levels
    Schumann, Ulrich
    Sharman, Robert
    [J]. JOURNAL OF AIRCRAFT, 2015, 52 (04): : 1277 - 1285
  • [6] Skill of an aircraft wake-vortex model using weather prediction and observation
    Frech, Michael
    Holzäpfel, Frank
    [J]. Journal of Aircraft, 1600, 45 (02): : 461 - 470
  • [7] Skill of an aircraft wake-vortex model using weather prediction and observation
    Frech, Michael
    Holzaepfel, Frank
    [J]. JOURNAL OF AIRCRAFT, 2008, 45 (02): : 461 - 470
  • [8] Numerical Optimization of Plate-Line Design for Enhanced Wake-Vortex Decay
    Stephan, Anton
    Schrall, Juergen
    Holzaepfel, Frank
    [J]. JOURNAL OF AIRCRAFT, 2017, 54 (03): : 995 - 1010
  • [9] Aircraft wake-vortex evolution in ground proximity: Analysis and parameterization
    Holzäpfel, Frank
    Steen, Meiko
    [J]. AIAA Journal, 2007, 45 (01): : 218 - 227