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Sheet 1

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25-27 January 2000. NASA's STEP for Aerospace Workshop at JPL. Sheet 1. ESTEC TOS-MC ... AAM, ARM, Mapping Table, AIM, Express-G (586 pages) ... – PowerPoint PPT presentation

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Title: Sheet 1


1
STEP for Space Applications -TAS and NRF
Development
  • Hans Peter de Koning (ESA/ESTEC
    D/TOS-MCV)hdekonin_at_estec.esa.int
  • Eric Lebègue (SIMULOG)Eric.Lebegue_at_esprico.fr

2
Topics of this presentation
STEP-NRF Network-model Results Format Application
Protocol
STEP-TAS Thermal Analysis for Space
Application Protocol
  • Overview of Application Protocols
  • Current status of implementations
  • Brief demo with ESARAD
  • STEP-TAS Converter Development Toolkit

3
NRF and TAS main documents
Definition and Results of Analyses, Tests
Operations Integrated Application Resource
Space Domain Integrated Application Resource
Thermal Analysis Integrated Application
Resource
STEP-NRF Network-model Results Format Application
Protocol
STEP-TAS Thermal Analysis for Space Application
Protocol
4
Application Reference Model Units of
Functionality
TAS space_mission_aspects geometric_model kinema
tic_model thermal_radiative_model visual_presentat
ion material_properties additional_physical_quanti
ties_and_measures
NRF product_structure network_model_representation
bulk_results parameterized_functions date_and_tim
e general_support
The ARM is organised in UoFs UoFs are collections
of application objects and their relationships
specified in the terminology of the application
domain
5
Main characteristics of NRF (1)
  • Generic discipline-independent protocol
  • Scope is definition and representation of
  • engineering objects represented by a
    network-model of discrete nodes and relationships
    between the nodes -network-model may contain a
    submodel hierarchy
  • representation of properties of engineering
    objects for which result values can be predicted
    / observed at discrete states
  • analysis, test or operational campaigns / cases /
    phases
  • analysis, test or operational runs with
    associated results
  • product structure compliant with AP203 CC1 / PDM
    schema
  • relationships between product structure and
    network-model

6
Main characteristics of NRF (2)
  • Results are properties with value and unit
  • Descriptive values (text string, item from
    enumerated list)
  • Numerical values (scalar, vector, tensor)
  • Parameterised function values (tabular
    interpolation, polynomial, limited expressions)
  • NRF protocol has two separate parts
  • Static protocol, discipline-independent data
    structures
  • Dictionairies defining node and node-relationship
    classes, properties, property-qualifiers,
    property-value-range, ...
  • Purpose of dictionairies is to enable flexible /
    adaptable use without need to re-issue the
    standard

7
Main characteristics of NRF (3)
  • Great care is taken to define light, efficient
    data structures
  • Sparsely populated results value space
  • Properties only one kind of unit in a data set
  • Starting on development of a best of both
    worlds solution
  • NRF for semantics
  • HDF5 for efficient binary portable implementation
    method (HDF Hierarchical Data Format by NCSA)

8
Main characteristics of TAS (1)
  • Self contained, complete Application Protocol
  • AAM, ARM, Mapping Table, AIM, Express-G (586
    pages)
  • Conforms to TC184/SC4 methods and guidelines
  • Geometry defined as AP203 CC4 surfaces
  • Thermal-radiative model faces added as associated
    features
  • Including possibility to support hierarchical
    submodel tree
  • Associated notional thickness, surface material
    and bulk material
  • Thermo-optical, thermo-physical properties for
    named material
  • Concept of material property environment (Part
    45)
  • Kinematic model conform STEP Part 105 for
    articulating rigid bodies (e.g. rotating solar
    arrays, gimballed antennas)

9
Main characteristics of TAS (2)
  • Space mission aspects
  • orbit arc (Keplerian and discrete ephemeris)
  • space co-ordinate system, celestial bodies
  • orientation, general and named pointing,
    spinning, linear rotation rates
  • space thermal environment, including constant or
    lat/long dependent albedo / planetshine tables
  • Boolean construction surfaces available for
    advanced tools
  • STEP-TAS CC1 Abstract Test Suite
  • conform STEP Part 3xx series
  • test suite has been used in validation of TAS
    processors

10
TAS geometry and thermal-radiative models
  • Shapes
  • Primitives triangle, rectangle, quadrilateral,
    disc, cylinder, cone, sphere, paraboloid
  • Compound shapes
  • Shapes conform to AP203 CC4 non-manifold surfaces
  • Thermal-radiative model
  • associates thermal-radiative faces with surface
    shapes
  • thermal mesh
  • surface and bulk material

11
Illustration of basic TAS Keplerian orbit
definition
12
STEP-TAS Conformance Classes
thermal-radiative model with basic geometry
kinematic model
constructive geometry
space mission aspects
CC-1
?
CC-2
?
?
CC-3
?
?
CC-4
?
?
?
CC-5
?
?
?
CC-6
?
?
?
?
13
STEP-NRF implementation status
  • Read/write library available with C and FORTRAN
    binding
  • Prototypes produced with CNES and Electricité de
    France
  • Being prepared for use in ESAs next generation
    integrated thermal analysis tool code-named
    Polytan as an open post-processing interface

14
STEP-TAS Implementation Status
  • Read/write libraries available with C and FORTRAN
    bindings
  • Including programming tutorials / manuals (HTML
    and PDF)
  • Ported and verified on 5 platforms PC/Windows,
    Sun/Solaris, HP/HP-UX, Compaq-Dec/Tru64, SGI/Irix
  • High level interface layer included at ARM/user
    domain level Provides very significant savings
    in processor development effort
  • Working processors
  • CC1 processor in ESARAD 4.1.x (released summer
    1999)
  • CC1 processor in THERMICA release April 2000
  • Currently large model cross validation ESARAD -
    THERMICA
  • Proof-of-concept prototypes developed with
    NASA-JPL for TRASYS and TSS (1998)

15
ROSETTA in ESARAD
16
ROSETTA in Baghera View
17
ROSETTA in THERMICA
18
Doris in THERMICA
19
Doris in Baghera View
20
DORIS in ESARAD
21
Mars Rover in TSS
22
Mars Rover in Baghera View
23
Mars Rover in ESARAD
24
Mars Rover in THERMICA
25
STEP-TAS future
  • STEP-TAS Processor Development Kit available to
    thermal analysis tool vendors
  • From SIMULOG at nominal cost EURO/USD 1000
    (Jan-2000) Including initial e-mail tech-support
  • Baghera View is available in addition (Contact
    Eric Lebègue)
  • ESA is considering proposing STEP-TAS to ISO
    TC184/SC4
  • New Work Item leading to new ISO 10303 part
  • Continue large model cross-validation and
    performance tuning
  • Initiate support for other conformance classes
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