1. STEP Protocol Development and Converter Implementation Processes at ESA Hans Peter de Koning - ESA/ESTEC - The Netherlands Hans-Peter.de.Koning@esa.int Sandrine Fagot - Simulog - France Sandrine.Fagot@simulog.fr STEP for Aerospace Workshop, NASA-JPL, 16-19 January 2001

2. Sheet 216-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Topics What is Europe doing w.r.t. standardisation of product data exchange & archival for space applications? How did we develop STEP based solutions? What successes? What lessons learned? Road ahead

3. Sheet 316-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL What is Europe doing? ECSS E-10-07 WG “Exchange of Product Data” –European Cooperation for Space Standardization –High level ‘meta-standard’ like NASA-STD-2817 www.estec.esa.int/ecss ftp://ftp.estec.esa.nl/pub/ecss-e-10-07-wg/index.html Specific standards –STEP-TAS “Thermal Analysis for Space” (ESA) –STEP-NRF “Network-model Results Format” (ESA) –STEP-PRP “Propulsion” (CNES) (CNES = French Space Agency ) –Active role AP232 “Technical Data Package” (CNES + Industry) –Active role AP233 “System Engineering” (Aerospace Industry) w.r.t. standardisation of product data exchange & archival for space applications

4. Sheet 416-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Focus of this presentation Development process of STEP-TAS and STEP-NRF Achievements, some metrics and lessons learned Objective: To provide useful feedback for others contemplating to develop similar ‘niche’/specific purpose standards

5. Sheet 516-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Main characteristics NRF (1) Network-model Results Format Targets engineering-discipline independent exchange of bulk results data from analysis, test or operation –Representation of engineering objects by network models consisting of discrete nodes and node-relationships –Hierarchical tree of network models / submodels –Definition of properties Quantitative, descriptive and functional properties Scalar, vector and tensor property values Property values only at discrete locations / discrete states –Full annotation of analysis / test / operation context Campaign, case, phase, run Facility/tool, environment, date and time, organisation, person,...

6. Sheet 616-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Main characteristics NRF (2) NRF dataspace abscissa_property model_component (model, node, node_relationship) state property_class Each gridpoint in the 3D dataspace is a property value Each can be scalar, vector, tensor Data model and implementation designed to handle sparsely populated dataspace efficiently

7. Sheet 716-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Main characteristics NRF (3) Proposed NRF/HDF architecture STEP-NRF protocol (discipline- independent) NRF Dictionary Structural NRF Dictionary Thermal NRF Dictionary Electrical NRF Dictionary... STEP-NRF SDAI programming library HDF 5 programming library NRF – HDF mapping HDF5 binary results file User Application (Reading or Writing Results Data) AP203 STEP file AP209 STEP file (future) reference to product (-part), shape, location reference to FEM / FE COTS or PD Data Analysis / Visualisation Application with HDF i/f (also via WWW) discipline-specific dictionaries HDF5 = Hierachical Data Format v5 - Public domain from NCSA - Efficient portable binary storage format - Full C, Fortran, Java libraries on >10 platforms - Standard for all NASA EOS missions and some ESA earth observation - Info/downloads at hdf.ncsa.uiuc.edu - Many COTS / PD tools with HDF interface HDF5 as an efficient alternative for Part21 for large amounts of similar data

8. Sheet 816-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Main characteristics TAS (1) Thermal Analysis for Space Self contained, complete Application Protocol –AAM, ARM, Mapping Table, AIM, Express-G –Conforms to TC184/SC4 methods and guidelines –Geometry defined conform AP203 CC4 surface model –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 articulated rigid bodies (e.g. rotating solar arrays,...)

9. Sheet 916-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Main characteristics 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 used in validation of TAS processors

10. Sheet 1016-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Main characteristics TAS (3) 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

11. Sheet 1116-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Brief history TAS and NRF developments 199019911992199319941995199619971998199920002001 SET-ATS precursor (French standard, CNES) ESA R&D project “Thermal neutral formats” TAS protocol (pure extension of NRF) Space IR and NRF protocol Programming libraries v1 with C & F77 API / porting 5 platforms Abstract test suite TAS-CC1 / roundtrip ESARAD/STEP-TAS Prototype NASA-JPL, import in TSS, export from TRASYS Editorial update protocol to TC184/SC4 MS-Word format Production release ESARAD/STEP-TAS-CC1 converter Porting F77 API 5 platforms; Thermica/STEP-TAS-CC1 converter (Astrium) US STEP-TAS pilot (JPL, 5 thermal tool vendors) Thermal Desktop/STEP-TAS-CC1 converter (C&R, NASA-LaRC) Large model cross validation ESARAD & Thermica; update architecture and libraries

12. Sheet 1216-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Challenge Find an effective development process –Within modest budget constraints –TAS for a ‘niche’ market Between 20 to ~300 real users per space thermal analysis tool –Make sure that user requirements are well captured –Ensure implementations can be, and are, validated –Facilitate efficient and maintainable converters –Attempt to obtain global consensus Ensure robustness and ease of use for end-users

13. Sheet 1316-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Incremental development scheme Define / Refine / Extend Protocol (ARM, AIM, Express) Develop / Upgrade Libraries Develop / Upgrade Converters & Test Suites Validate Converters with Test Suites

14. Sheet 1416-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Stable Team with Clear Roles Simulog (F, software engineering services) –lead since 1998, implementation libraries and some converters Fokker Space (NL, space subsystems contractor) –initial lead, user requirements, ARM, ATS GOSET (F, STEP standardisation experts) –mapping table, AIM, EXPRESS/p21 verification Epsilon Ingénierie (F, thermal analysis services) –check user requirements, converter implementation ALSTOM Power (UK, thermal tool vendor) –converter implementation, distribution to end-user CNES (F, French Space Agency) –Review requirements and model, generation of test suites

15. Sheet 1516-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Approach to Developing with STEP Be as precise as possible on semantics –Regular feedback between protocol editor and implementors Minimise ARM - AIM mapping need as much as possible –Use IR contructs where possible direct in ARM Automate generation of library APIs as much as possible –Directly from EXPRESS model Design for simplicity, implementability and testability –E.g. do not use EXPRESS ANDOR Use a high level programming interface to build converters Use an SDAI toolkit for low level interface

16. Sheet 1616-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL STEP-TAS High Level Libraries Toolkit High-level API to support efficient converter development –Use ARM constructs - close to thermal developer’s data model –Hide STEP complexity –Full set of reading / writing functions in ANSI-C and F77 –Associated documentation, examples and test suite BagheraView ( CNES ) included to perform independent visual inspection and model reporting on PC/Windows Distribute toolkit at nominal cost to attract tool vendors API = Application Programming Interface

17. Sheet 1716-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL BagheraView Screenshot

18. Sheet 1816-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Benefits of High Level Libraries Approach Already ported and tested with target compilers –PC/Windows, Sun/Solaris, HP/HP-UX, Compaq/Tru64, SGI/Irix Enables to jumpstart converter implementation Reduces converter validation / verification effort All converters share reading/writing interface –implementation mismatch is minimised –increased reliability Extensibility at affordable cost –e.g. to add HDF or XML encoding

19. Sheet 1916-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL STEP-TAS EXPRESS data model STEP-TAS EXPRESS data model STEP-TAS physical file (ISO 10303-21) STEP-TAS physical file (ISO 10303-21) Thermal Analysis Tool (ESARAD, THERMICA, TRASYS, …) Thermal Analysis Tool (ESARAD, THERMICA, TRASYS, …) STEP-TAS High Level Libraries C and Fortran API (Simulog, France) STEP-TAS High Level Libraries C and Fortran API (Simulog, France) SDAI C Library (ISO 10303-24) ST-Developer (STEP Tools Inc., USA) SDAI C Library (ISO 10303-24) ST-Developer (STEP Tools Inc., USA) STEP-TAS Converter Architecture Native Tool Format Native Tool Format

20. Sheet 2016-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Successes … Full implementation of converters at reasonable cost –ESARAD/STEP-TAS-CC1 since mid 1999 –Thermica/STEP-TAS-CC1 since Dec 2000 Broad awareness and (prototype) implementation in US –JPL STEP-TAS demonstrator in 5 US thermal tools –Full bi-directional implementation STEP-TAS-CC1 in Thermal Desktop 3.3Beta (Cullimore & Ring sponsored by NASA-LaRC) Reached almost 100% of space thermal tool vendors Very close to robust and reliable quality exchange for STEP-TAS-CC1 in production tools

21. Sheet 2116-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL … Problems with STEP Bulkiness and incomprehensibility for humans of AIM Makes validation cumbersome and costly Causes large overheads Additional in-core storage Addition interface layer in library Part21 files much larger than really really necessary ARM to AIM mapping is not computer interpretable EXPRESS-X was not available for TAS: a lot of handwork for high level library interface mapping Conformance checking / Abstract Test Suite (Parts 3x) Very cumbersome and costly to develop and maintain Not well designed for automation of regression testing

22. Sheet 2216-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Lessons Learned Iterative, incremental development necessary –Can not get things right in one go … High level programming library very useful –Greatly reduces converter development effort –Speeds up standard penetration & increases exchange reliability –Chosen API close to old SET-ATS interface needs reconsideration Continuous resource / funding level is needed –To meet vendor expectations by providing timely support and library updates resolving SPRs Communication must be improved –Start a ‘STEP-TAS implementors forum’ ?

23. Sheet 2316-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Metrics STEP-TAS took ~5 years from conception to CC1 industrial converter release Up to now funded with roughly 1 million Euro / USD –Excluding US converter developments –Appears to be a quite good price/performance ratio Approximately 20 different people have worked on different parts of STEP-TAS and STEP-NRF

24. Sheet 2416-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Why was STEP-TAS not yet submitted as an ISO TC184/SC4 work item? Valid question Started as a European effort to follow up SET-ATS Limited resources prevented us to bear the additional effort of formal ISO standardisation - no added value yet With the good co-operation with NASA in place, nearly 100% of the space thermal tool vendors in the world were reached However it is agreed that a formal way of publishing and maintaining the standard is now needed imminently

25. Sheet 2516-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Road Ahead (1) Web-based collaboration on further development –ftp://ftp.estec.esa.nl/step-tas/index.html as a start –Publication of protocol, SPR list, test suite –FTP distribution of STEP-TAS toolkit releases –E-mail tech support Take European / US collaboration to a next stage –Action ESA and NASA together with Simulog –Clarify/establish intellectual property rights and support

26. Sheet 2616-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Road Ahead (2) Currently trade-off for ‘Return on Investment’ next 5 years –Appropriate level of formal publishing (ISO?, ECSS?, NASA?) –Select AIM or ARM based exchange? –Upgrade high level API to support all STEP-TAS constructs e.g. submodelling, non-uniform meshing and node numbering Upgrade libraries to resolve all reported issues (SPRs) Upgrade converter options –Consistently support length unit selection / conversion –Meta data entry

27. Sheet 2716-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Road Ahead (3) TRASYS/STEP-TAS-CC1 bi-directional converter –Stand-alone tool by Simulog on ESA funding –Will be made available at nominal cost or preferrably free Upgrade BagheraView capabilities –By Simulog sponsored by CNES PATRAN/STEP-TAS-CC1 interface –By MSC sponsored by NASA-LaRC Continue NRF developments –HDF5 binding (co-operation with EDF, NCSA and others) –Assess links with Engineering Analysis modules, ISO 10303-50 –Pilot web-based remote consultation of structural test results

28. Sheet 2816-19 Jan 2001STEP for Aerospace Workshop - NASA-JPL Acknowledgements STEP-TAS and STEP-NRF were developed under ESA contract by an industrial consortium, consisting of: –Simulog (F, prime) –Fokker Space (NL) –Association GOSET (F) –Epsilon Ingénierie (F) –Alstom Power (UK) and supported by CNES (F) Special thanks to Georg Siebes (NASA-JPL) who is and has been the driving force for the development and acceptance of STEP-TAS in the US Also acknowledgements to Ruth Amundsen (NASA-LaRC) for actively promoting STEP-TAS implementations