SVIL GPSIIR Modernization Using NI Technology
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1 SVIL GPSIIR Modernization Using NI Technology 2012 FSW Workshop November 7, 2012 Anthony Vescovi 1 1
2 SVIL Business Case - Executive Summary Four foundational SVIL capabilities promise to increase execution efficiency and lower program costs: 1. Model-Based Graphical Software with Autocode capability for Embedded Systems Software 2. Low-Cost Test Beds introduced early in the lifecycle that fill a crucial gap in a suite of simulation capabilities currently on typical programs 3. Risk Reduction testing using Rapid Prototyping with Models and Test Beds in critical risk areas 4. Early Lifecycle Testing on heritage and new software products to gain customer confidence and mature the end software product 2 2
3 SSIM-B #2 SVIL Architecture, Products & Services SW Development Models IO Drivers Utilities Integration Models CDH C&DH & FSW Telemetry Processing CMD Distribution Logging Utility DMS Utility SV Models Selected Component Models Timing Utility Logging Utility DMS Utility SimCmd /Tlm I/O Manager I/O Manager SVIL Development Team Test Software framework FSW Framework Tlm Processor Cmd Processor Task Scheduler Middleware Middleware Reflective SpaceWire SpaceWire Shared Reflective Memory Driver TCP/IP Driver Driver Driver Memory Memory Engineering Flight Commands Development Sim Command and and Telemetry Path Unit (EDU Telemetry Path TLMScope CMDBuilder TLMScope CMDBuilder AF C&C Manager C&C Manager AF Tools Test Manager Test Manager Tools LMI SVIL Environment Simulator HW Loaded on Simulator HW Simulation Users IT Infrastructure Flight EDU s Simulator Debug/Analysis Tools 3 3
4 Project Background GPSIIR SPU/STE simulation platform for validating FSW prior to uploading to on orbit satellite GPSIIR STE Enhancements Current Hardware Architecture: STE Specialized Test Equipment SPU Spacecraft Processing Unit 4 4
5 Current System Architecture STE Hardware Custom I/O Boards: 2 Digital Chassis Units 1 Analog Chassis Units STE to SPU Interface SPU Power SPU Power Distribution Unit Voltage Test Points STE Computer HP1000 A990 Or PC-based Kestrel QX HP1000 A990 emulator HP I/O cards 11 Parallel 1 12-bit d/a Computer to STE Interface GPSSIM Environmental and spacecraft sensor/actuator models 5 5
6 Current STE Computer HP 1000 A990 Functions as I/O host for STE Circa 1990 hardware/software HP parallel interface cards Not easily configurable Must disable certain features to test flight software, can t test like you fly Requires unique skill sets 6 6
7 GPSIIR Architecture Trades Solution #1 Hardware Interface Box (HIB) Not deterministic Not enough TTL I/O Want a solution we can maintain ourselves Need better growth potential 7 7
8 GPSIIR Architecture Trades Solution # 2 - VME COTS FPGA Integration relatively difficult Requires traditional development toolsets Low backplane throughput Less growth capability 8 8
9 GPSIIR Architecture Trades Solution #3 NI PXIe System Easiest FPGA Integration Simplified Technical Design Much higher throughput than we need room to grow Point to point bus topology More Rapid Development Time One environment - LabView Free from burden of low level software elements Focus effort on specific challenges related to program Prototyped with multiple architectures 9 9
10 System Architecture STE Hardware Custom I/O Boards: 2 Digital Chassis Units 1 Analog Chassis Units STE to SPU Interface SPU Power SPU Power Distribution Unit Voltage Test Points NI PXI Chassis PXI Controller running LV Realtime NI I/O FPGAs Analog Input Computer to STE Interface GPSSIM Environmental and spacecraft sensor/actuator models 10 10
11 System Architecture Typical Real Time/FPGA Architecture External Command Host Real Time Controller 7854R RIO FPGAs 6255 Analog Input Card 11 11
12 NI Support Loaner equipment Lowers cost Removed procurement from development process Technical Support Design Reviews 12 12
13 Maintenance NI Premium System Assurance 5 year warranty service After warranty period system evaluated for active products 5 years calibration NI Yearly Software Support Plan 13 13
14 STE Enhancements Reduced risk to on-orbit assets Faster patch development & validation Test like you fly No longer will need to disable large portions of FSW to run on SPU-STE Patches can be fully validated on ground 14 14
15 SVIL Benefits Introduces new capability to SVIL Simulator domain Pioneering LabVIEW and NI hardware for HWIL testing Entry into adjacent market New product possibilities Potential for growth and expanded capabilities 15 15
16 16
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