Evolution of Software-Only-Simulation at NASA IV&V
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1 Evolution of Software-Only-Simulation at NASA IV&V Justin McCarty Justin Morris Scott Zemerick NASA IV&V Facility 100 University Drive Fairmont, WV 26554
2 Agenda Introduction to Software-Only-Simulation Process and approach for simulation and hardware modeling Independent Test Capability (ITC) Jon McBride Software Testing & Research Lab (JSTAR) Infrastructure, Deployment, and Users Technologies Developed Development Evolution of Spacecraft Simulators Closing Remarks Lessons Learned 2
3 Software-Only-Simulation Introduction 3
4 Software-Only-Simulation is a complete software representation of modeled hardware components and software emulators Together, the components form a complete spacecraft simulator Software-Only-Simulator provides complete control of CPU, Time, and Memory Can stop all execution for debugging. Can peek/poke memory, perform fault injection Spacecraft simulator used for: Independent Testing (IVV) Operator Training Augment Project Hardware Testing Software-Only-Simulation Introduction 4
5 Software-Only-Simulation Introduction Simulator Components Modeled Spacecraft Hardware cpci, Spacewire, 1553, Ka-band, S-band, FPGAs, etc Instruction Set Simulator Simics/Qemu ppc750, ppc401, LEON3, etc Unmodified Flight Software Binary Independent Testing Halt Entire System Memory Analysis Fault Injection Operational Ground System Spacecraft Scenarios What-IF Scenarios Operator Training 5
6 Software-Only-Simulation Introduction Simulator Development Process 6
7 NASA IV&V Independent Test Capability (ITC) Introduction 7
8 Independent Test Capability (ITC) Introduction Charter Acquire, develop, and manage adaptable test environments that enable the dynamic analysis of software behaviors for multiple NASA missions Dynamic Analysis is performed on flight software to verify software behavior 8
9 ITC Develops System Simulators Independent Test Capability (ITC) Introduction Experts in Hardware Modeling and Distributed Simulation Experts in Simulator & Software Integration 9
10 Jon McBride Software Testing & Research (JSTAR) Laboratory Cloud-based infrastructure using server and desktop virtualization Large scale simulator deployments Hardware-in-the-loop and software-only test environments Integration of COTS and GOTS software tools to support V&V activities 10
11 Jon McBride Software Testing & Research (JSTAR) Laboratory Virtualized Deployment 11
12 ITC Technologies 12
13 Software-only simulation architecture NASA Operational Simulator (NOS) Capable of executing unmodified flight software Custom layered-architecture middleware Dynamic interception capability Reusable software modules and scripts Virtual machine deployment ITC Technologies Typical NOS Architecture (Space Domain) 13
14 NOS Feature Set Plug-and-Play Hardware Models Processors, Boards, Racks Use of Operational Ground Systems Software Instrument Model Framework Instrument1 Subaddress HandlerA FunctionA Subaddress HandlerB FunctionB Subaddress HandlerN FunctionN InstrumentX Subaddress HandlerA FunctionA Subaddress HandlerB FunctionB Subaddress HandlerN FunctionN Internal Bus Monitoring NOS Middleware Deployment & Maintenance Specialized Layers Base Layer Communications Virtualization 14
15 NOS Middleware Overview Offers re-usable communication mechanism Ensures consistent and correct data passing Provides synchronization between distributed applications Flexible and extensible design Can be extended to incorporate any communication protocol Features Transport agnostic Cross platform C++ implementation Robust User API Specialized User API Layers MIL-STD-1553B ESA SpaceWire Discrete Signals Time Synchronization Interception allows for V&V analysis No modification to softwareunder-test 15
16 NOS Middleware Architecture System Under Test MIL-STD-1553 SpaceWire Discrete NOS Core Middleware with Interception Capability Time Synchronization Additional Protocols as Needed System Monitoring Bus Analyzer I/O Interface Layer 16
17 NOS Software Utilities Virtual Oscilloscope Virtual CompactPCI (cpci) Analysis Board-Level Signal Analysis Virtual MIL-STD-1553 Bus Bus Controller with XML Defined Schedules Remote Terminal Bus Monitor/Logger PASS3200 Software Emulator Virtual SpaceWire Router 17
18 NOS Dynamic Interception Interceptor Data Flow Modifying With Normal Data Blocking Flow Interceptor Data Node A NOS Node B Modify Block Interceptor 18
19 Evolution of ITC Spacecraft Simulators 19
20 Evolution of ITC Spacecraft Simulators Global Precipitation Measurement (GPM) Operational Simulator (GO-SIM) Closed-loop simulator including unmodified operational ground system, unmodified flight software, environmental simulator, and science instrument simulators James Webb Space Telescope (JWST) Integrated Simulation and Test (JIST) Simulator that demonstrates reusable NOS technologies can be applied to other NASA missions Deep Space Climate Observatory (DSCOVR) Turn-key modeling effort for spacecraft C&DH 20
21 Evolution of ITC Spacecraft Simulators GPM Operational Simulator (GO-SIM) 21
22 GPM Operational Simulator GO-SIM Components Capabilities COTS Emulator Primary Instrument Simulations (GMI/DPR) GPM Ground System GSFC Goddard Dynamic Simulator (GDS) NOS Middleware GPM Hardware Models Load and run unmodified flight software binaries Execute test flight scripts Single-step debugging Inject errors via ground system and NOS middleware Stress system under test 22
23 GO-SIM Architecture ASIST Ground System with FEDS SCOMM Simulator RAD 750 Emulator GPM FSW SpaceWire Router NOS Middleware KEY TCP/IP 1553 SpaceWire 1553 & SpaceWire 23 Dynamics Simulator (GDS) Instrument Simulator (GMI) Instrument Simulator (DPR) 23
24 Evolution of ITC Spacecraft Simulators James Webb Space Telescope (JWST) Integrated Simulation and Test (JIST) 24
25 Software-only spacecraft simulator Flexible environment to support V&V activities Unmodified ground system and scripts Unmodified software-under-test binaries Integration of COTS, GOTS and in-house developed components Custom hardware models Automated Testing Framework Fault Based Testing JWST Integrated Simulation and Test (JIST) 25
26 JIST Architecture ECLIPSE CCTS Ground System Ground System Simulators (MTTS/TCTS) Comm Cards RAD 750 Emulator PPC 405 Emulator NOS Middleware KEY TCP/IP 1553 Shared Memory 1553 & SpaceWire Instrument Simulations (DSIM) Solid State Recorder Simulation Dynamics Simulator RAD750 Emulator ISIM FSW 26
27 JIST Architecture 27
28 Evolution of ITC Spacecraft Simulators Deep Space Climate Observatory (DSCOVR) 28
29 DSCOVR Architecture 29
30 Simulator Level-of-Effort Comparison Year Usage Simulator Effort Prototype (Basic C&DH) Complexity Users GO-SIM 2 FTEs 6 Months Medium IV&V, GPM Project Testers Launch Support Ongoing JIST 2 FTEs 4 Months Very High IV&V, JWST Test Labs, JWST Operations Ongoing DSCOVR 1 FTE 2 Months Low DSCOVR Testers DSCOVR Operations 30
31 Evolution Lessons Learned Establishment of a reusable simulation architecture has proven to save costs and reduce future effort Automate tests and deployments as much as possible as it allows for engineers to focus on more challenging tasks Hardware modeling should focus on the minimum needed in order for the flight software to execute. Establish this baseline then augment to support full V&V dynamic testing using an iterative process. Spend considerable time writing unit tests for the hardware models. When things go wrong, debugging is very difficult. Integration of simulators to form a system will require significant development labor, cost, and time. 31
32 Contact Information Web Page Contact us for Demonstrations of test beds Middleware usage agreements Simulator development Hardware modeling V&V Services, HWIL Testing, Performance Testing 32
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