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MDOB Overview

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for the design of complex engineering systems and subsystems. that coherently exploits the mutually interacting subsystems' synergism. Analysis and ... – PowerPoint PPT presentation

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Title: MDOB Overview


1
MDOB Overview
  • Dave Rudy
  • Assistant Head, MDOB

Integrated Design Center Meeting Feb. 27, 2003
2
MDO Definition
  • Multidisciplinary Design Optimization (MDO) is
  • a collection of methodologies
  • for the design of complex engineering systems and
    subsystems
  • that coherently exploits the mutually interacting
    subsystems synergism

3
MDR Conceptual Elements
Analysis and Approximations
Organization and Culture
Design Problem Formulations and Solutions
Information Processing and Management
Cost-fidelity trade-off
Design problem formulation
Software engineering
MD Training
Approximations
Problem de- /re- composition
Data and software standards
MD process insertion
High-fidelity results inclusion
Optimization algorithms
Data visualization, storage, management
MD in integrated product teams
Parametric product data models
Optimization procedures
MD environment
MD in existing organization
SD analysis and sensitivity analysis
SD optimization
Human interface
  • based on Special Session on Industry Needs at
    1998 AIAA/MAO (AIAA Paper 98-4737)

MD analysis and sensitivity analysis
MD optimization
MD computing
4
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6
Approximation Management
  • Accomplishment
  • A rigorous mathematical framework was developed
    for exploiting low-fidelity models to reduce the
    cost of high-fidelity optimization while still
    obtaining the correct optimum
  • Demonstrations for aerodynamic optimization have
    been made for various types of low-fidelity
    models, including response surfaces, coarse grids
    and simpler physics
  • Significance
  • Navier-Stokes optimization using unstructured
    grids was sped up by a factor of 5 for
    multi-element airfoils and by a factor of 3 for
    3-D wings
  • This approximation and model management framework
    is used in LaRCs FAAST project for reducing the
    time of CFD analysis and design

7
3D Aerodynamic Design with AMMO
  • Accomplishments
  • Implemented efficient FUN3D-based aerodynamic
    optimization by judicious combination of
    higher-fidelity NS analyses and lower fidelity
    Euler analyses.
  • Significance
  • Greatest expected benefit of AMMO is in reducing
    the cost of extremely expensive, 3D design
    problems this implementation demonstrated
    approximately a 4-fold saving in high-fidelity
    analyses and sensitivity analyses
  • Confirms results obtained earlier with FUN2D and
    CFL3D

8
CAD-Based Cost Estimation for a BWB
  • Accomplishments
  • Process assesses manufacturing cost for novel
    vehicle concepts
  • Manufacturing cost models based on 10 years of
    NASA investment in physics-based manufacturing
    cost model.
  • Significance
  • Physics-based cost models provide realistic
    estimates for novel vehicle concepts
  • Enabling technology brings manufacturing cost
    considerations directly into conceptual design
    processes.

9
Rapid Generation of Feasible Conceptual
Spacecraft Designs
  • Accomplishments
  • Automation of process and addition of a genetic
    algorithm to SmallSAT enable very rapid
    examination of many diverse combinations of
    spacecraft design variables
  • Significance
  • No conceptual spacecraft design tools known to
    have this automated capability.
  • GA can be integrated with a conceptual spacecraft
    design tool in a Windows NT spreadsheet
    environment.

10
Legacy Code IntegrationApplication Trimmed
Aeroelastic Analysis
  • Accomplishment Description
  • Used Rational Unified Process to capture software
    requirements
  • Developed integrated process from 25 individual
    lower level processes
  • Implemented with UNIX Script, Python Script, and
    Model Center
  • Significance
  • Demonstrated disciplined yet fast turnaround
    integration approaches to successfully integrated
    off-the-shelf codes

11
Probabilistic RLV Design
  • Accomplishment Description
  • Tracked uncertainties due to variability in shape
    variables and uncertainty in aerodynamic
    parameters on minimum weight and pitching
    constraint.
  • Demonstrated the sensitivities of the pitching
    moment constraint at Mach 10 to the uncertain
    aerodynamic data.
  • Significance
  • Application to conceptual multidisciplinary
    design
  • Probabilistic formulation of design for
    controllability

12
In Conclusion
  • Visit us at http//mdob.larc.nasa.gov
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