GLAST Large Area Telescope LAT Flight Software System Checkout TRR Test Suites (Backup) Stanford Linear Accelerator Center Gamma-ray Large Area Space Telescope.

Slides:



Advertisements
Similar presentations
System Integration and Performance
Advertisements

GLAST LAT ProjectManager’s Face to Face - ISOC, 17 March GLAST Large Area Telescope WBS 4.1.B Instrument Science Operations Center Manager’s Face.
1 GLAST Large Area Telescope Monthly Mission Review LAT Flight Software Status June 6, 2007 Jana Thayer Stanford Linear Accelerator Center Gamma-ray Large.
GLAST LAT Project I&T Integration Kickoff Meeting 03/09/04 Online 1 GLAST Large Area Telescope: I&T Integration Kickoff Meeting EGSE Hardware March 9th,
GLAST LAT ProjectOnline Peer Review – July 20, Integration and Test R. Claus 1 GLAST Large Area Telescope: I&T Integration Readiness Review.
GLAST LAT ProjectLAT Engineering Meeting, April 1, 2003 GLAST Large Area Telescope: Performance & Safety Assurance Darren S. Marsh Stanford Linear Accelerator.
GLAST LAT ProjectISOC CDR, 4 August 2004 Document: LAT-PR-04500Section 3.11 GLAST Large Area Telescope: Instrument Science Operations Center CDR Section.
GLAST LAT Project LAT System Engineering 1 Test Definition Planning Pat Hascall SLAC System Engineering Gamma-ray Large Area Space Telescope.
1 GLAST Large Area Telescope Monthly Mission Review LAT Flight Software Status May 2, 2007 Jana Thayer Stanford Linear Accelerator Center Gamma-ray Large.
GLAST LAT ProjectISOC Peer Review - March 2, 2004 Document: LAT-PR Section 2.1 Requirements 1 Gamma-ray Large Area Space Telescope GLAST Large.
GLAST Large Area Telescope Instrument Flight Software F2F Meeting March 17, 2005 Jeff Fisher FSW Manager Stanford Linear Accelerator Center Gamma-ray Large.
RFA 18 – Automation of Operations Software Specific Request –Specify plans and requirements for automation of operations software, and describe the software.
GLAST LAT ProjectGLAST Flight Software IDT, October 16, 2001 JJRussell1 October 16, 2001 What’s Covered Activity –Monitoring FSW defines this as activity.
GLAST LAT Project ISOC Peer Review - March 2, 2004 Document: LAT-PR Section 2.3 Verification and Validation 1 Gamma-ray Large Area Space Telescope.
Section 15-1GLAST Ground System Design Review August 18&19, 2004 ISOC Organization ISOC Manager R Cameron Commanding, H&S Timeline Planning Command Generation.
GLAST LAT Project ISOC Peer Review - March 2, 2004 Document: LAT-PR Section 3 LOF Operations Concept 1 Gamma-ray Large Area Space Telescope GLAST.
GLAST LAT ProjectISOC CDR, 4 August 2004 Document: LAT-PR-04500Section 4.11 GLAST Large Area Telescope: Instrument Science Operations Center CDR Section.
GLAST LAT Project Quarterly Review, Aug. 14, 2001 Gunther Haller1 GLAST Large Area Telescope: Electronics, DAQ & Flight Software Gunther Haller Stanford.
GLAST LAT ProjectISOC CDR, 4 August 2004 Document: LAT-PR-04500Section 21 GLAST Large Area Telescope: Instrument Science Operations Center CDR Section.
GLAST LAT Project28 March 2005 LAT System EngineeringLAT Test Planning Meeting GLAST LAT GLAST LAT System Engineering Gamma-ray Large Area Space Telescope.
ISOC Peer Review - March 2, 2004 Section GLAST Large Area Telescope ISOC Peer Review Test Bed Terry Schalk GLAST Flight Software
GLAST LAT Project Oct 5, GLAST Large Area Telescope Systems Engineering Test Status, NCRs and Verification Status Pat Hascall Systems Engineering.
GLAST LAT ProjectNovember 18, 2004 I&T Two Tower IRR 1 GLAST Large Area Telescope: Integration and Test One and Two Tower Integration Readiness Review.
GLAST Large Area Telescope ISIS Post Acceptance Test Review 28 January 2005 ISIS Completion Status Jana Thayer Stanford Linear Accelerator Center
GLAST Large Area Telescope Instrument Flight Software Flight Unit Design Review 16 September 2004 Telecommand and Telemetry Data Dictionary Services Sergio.
GLAST Large Area Telescope LAT Flight Software System Checkout TRR Current Status Sergio Maldonado FSW Test Team Lead Stanford Linear Accelerator Center.
1. 2 Purpose of This Presentation ◆ To explain how spacecraft can be virtualized by using a standard modeling method; ◆ To introduce the basic concept.
Chapter 3: Operating-System Structures System Components Operating System Services System Calls System Programs System Structure Virtual Machines System.
GLAST Large Area Telescope Instrument Flight Software Flight Unit Design Review 16 September 2004 LAT Housekeeping Sergio Maldonado Stanford Linear Accelerator.
GLAST LAT ProjectDOE/NASA Peer Review, March 19-20, 2003 GLAST Large Area Telescope: Electronics, Data Acquisition & Instrument Flight Software Flight.
GLAST Large Area Telescope Instrument Flight Software Flight Unit Design Review 16 September 2004 Primary Boot Code (PBC) D. Wood Naval Research Laboratory.
IES Flight Software J. Hanley / P. Mokashi May 29, 2013.
GLAST Large Area Telescope Instrument Flight Software Flight Unit Design Review 16 September 2004 Diagnostics Framework James Swain Stanford Linear Accelerator.
GLAST LAT ProjectEGSE Peer Design Review, August 17, S. WilliamsEGSE Overview Electrical Ground Support Equipment Overview Scott Williams Stanford.
GLAST LAT Project4 April 2005 LAT System EngineeringLAT Test Planning Meeting GLAST LAT GLAST LAT System Engineering Gamma-ray Large Area Space Telescope.
GLAST Large Area Telescope Instrument Flight Software Flight Unit Design Review 16 September 2004 Software Watchdog Steve Mazzoni Stanford Linear Accelerator.
GLAST LAT ProjectDOE/NASA Peer Review, March 19-20, 2003 GLAST Large Area Telescope: Electronics, Data Acquisition & Instrument Flight Software Flight.
GLAST LAT Project Technical/Cost/Schedule Review 06/30/ Integration and Test 1 GLAST Large Area Telescope: I & T Input to Monthly Technical/Cost/Schedule.
Aquarius Mission Simulation A realistic simulation is essential for mission readiness preparations This requires the ability to produce realistic data,
GLAST LAT Project LAT System Engineering 1 GLAST Large Area Telescope: LAT System Engineering Pat Hascall SLAC System Engineering Manager
GLAST Large Area Telescope LAT Flight Software System Checkout TRR Systems Engineering Mike DeKlotz GSFC Stanford Linear Accelerator Center Gamma-ray Large.
GLAST Large Area Telescope Flight Unit Peer Review 16 September 2004 Flight Software Testing Eric Hansen Stanford Linear Accelerator Center
GLAST Large Area Telescope Instrument Flight Software Flight Unit Design Review 16 September 2004 Instrument Configuration James Swain Stanford Linear.
LAT ISOCISOC Review, 15 February GLAST Large Area Telescope Instrument Science Operations Center Commanding, Health and Safety Rob Cameron Stanford.
1. 2 Purpose of This Presentation ◆ To explain how spacecraft can be virtualized by using a standard modeling method; ◆ To introduce the basic concept.
GLAST LAT ProjectISOC CDR, 4 August 2004 Document: LAT-PR-04500Section 3.21 GLAST Large Area Telescope: Instrument Science Operations Center CDR Section.
Tracing the JWST Proposal from User Interface to Commanding of an Instrument Margaret Meixner & WIT Balzano, Robinson & CMD.
GLAST LAT ProjectCDR/CD-3 Review May 12-16, 2003 Document: LAT-PR Section 5 IOC Subsystem 1 GLAST Large Area Telescope: IOC Subsystems WBS: 4.1.B.
NICMOS Suspend Event STB 632 “MECH_2_MAX_RETRIES_EXCEEDED” 2008/069.
GLAST Large Area Telescope Instrument to Spacecraft Interface Simulator (ISIS) Test Readiness Review 15 December 2004 Jana Thayer Eric Hansen Stanford.
GLAST Large Area Telescope LAT Flight Software System Checkout TRR FSW Overview Sergio Maldonado FSW Test Team Lead Stanford Linear Accelerator Center.
GLAST Large Area Telescope LAT Flight Software System Checkout TRR Test Environment Sergio Maldonado FSW Test Team Lead Stanford Linear Accelerator Center.
GLAST Large Area Telescope Instrument Flight Software Flight Unit Design Review 16 September 2004 Secondary Boot Code (SBC) D.Wood Naval Research Laboratory.
GLAST Large Area Telescope LAT Flight Software System Checkout TRR Software Quality Assurance Kelly Burlingham SQE Stanford Linear Accelerator Center Gamma-ray.
GLAST LAT ProjectDOE/NASA Peer Critical Design Review, March 19-20, 2003 D. Nelson 1 GLAST Large Area Telescope: Electronics, Data Acquisition & Instrument.
GLAST Large Area Telescope Instrument Flight Software Flight Unit Design Review 16 September 2004 Instrument Configuration by File James Swain Stanford.
GLAST LAT ProjectSLAC Internal Review, April 16-18, 2002 LAT-PR Electronics and Flight Software WBS GLAST Large Area Telescope: Electronics,
EMI/EMC GLAST Large Area Telescope LAT Pre-Shipment Review
I&T&C Organization Chart
GLAST Large Area Telescope:
Chapter 2: System Structures
GLAST Large Area Telescope
Electrical Ground Support Equipment Verification Test Support
Launch and On-orbit Checkout
GLAST Large Area Telescope:
LAT Operations Scenario Subsystem Meetings
GLAST Large Area Telescope
GLAST Large Area Telescope
GLAST Large Area Telescope
GLAST Large Area Telescope:
Presentation transcript:

GLAST Large Area Telescope LAT Flight Software System Checkout TRR Test Suites (Backup) Stanford Linear Accelerator Center Gamma-ray Large Area Space Telescope

September 16, 2005 FSW System Checkout TRR: Test Suites 2 Test Suites CMDFNC - Command Functional –Verifies telecommands and telemetry can be exchanged across the 1553 interface between the spacecraft and the LAT –Verifies that all LAT commands are exercised through the 1553 interface, at a rate of up to 20 commands per second, with command execution and completion status reported in telemetry when command verification features are switched on –Verifies that the FSW validates commands and command parameters prior to command execution –Verifies that FSW responds properly to valid boot-related and a subset of telecommands not validated in other test suites –Verifies that invalid telecommands of all types are correctly rejected by FSW –Verifies that SIU FSW receives the information contained in the Timetone, Attitude, and Ancillary data messages from the spacecraft

September 16, 2005 FSW System Checkout TRR: Test Suites 3 Test Suites (2) DCMODE – Diagnostic Mode –Verify that the SIU FSW properly transitions to diagnostic mode upon command, then properly executes the requested diagnostic algorithms. EVTFIL – Event Filtering –Verifies that fully assembled, properly formatted events are received directly into EPU memory, where they can be processed by EPU FSW –Verify that the filtering algorithms provide acceptable results for a set of scenarios derived from Monte Carlo simulations –Verify that the filter software can pass a pre-scaled sample of unfiltered events on command –Verifies that the filter may be reprogrammed via the SIU, and that any changes to the filter configuration are reported in telemetry

September 16, 2005 FSW System Checkout TRR: Test Suites 4 Test Suites (3) EVTPMO – Event performance monitoring –Verify that the FSW operates properly in every science mode, monitoring event data for integrity, tracking changes in event and detector statistics, generating a report of any detected anomalies, as well as monitoring deadtime (during normal observations and during GRB observations) and reporting deadtime statistics in telemetry FECALB – Charge injection calibration –Verify that the FSW properly transitions to calibration mode upon command, then properly executes the requested calibration algorithms according to configurations read from the CPU file system –Verify the end-to-end processing of a known pattern of data from the LAT electronics to the EPUs FILMGT – File Management –Verify that the FSW can, on command, report file system status, create and delete file directories, dump directories, delete files, copy files (on a single SIU or EPU, and from an SIU to an EPU), dump files and file directories, load files during (SIU) primary boot and application modes, and cancel active file uploads

September 16, 2005 FSW System Checkout TRR: Test Suites 5 Test Suites (4) FSWINI – FSW initialization –Verify that the SIU and EPU(s) can be correctly booted and that during boot, the FSW boot code can calculate boot image checksums, perform memory scrubbing, and carry out other required error mitigation procedures; report system errors during primary boot in housekeeping telemetry; establish a reference state based upon information in nonvolatile storage; signal boot status over a discrete line to the spacecraft (SIU only); and then, power and initialize the remaining LAT subsystems in an orderly manner, resulting in a known reference state at the end of the process –Verify that the SIU and EPU(s) can write a boot error log and return the contents of the log in telemetry, on command. –Verify the mechanisms for recovery should the LAT or one of its processors become non-operational or lose communications, either internally or with the spacecraft –Verify compliance with all reboot requirements IPCFNC – SIU to EPU Communications –Verifies the LATp communications protocol for sending and receiving information between the CPUs, including timing, acknowledgments, and other transport level functions

September 16, 2005 FSW System Checkout TRR: Test Suites 6 Test Suites (5) MEMMGT – Memory Management –Verify that FSW can successfully upload data into a specified block of CPU memory and verify the correct memory contents –Demonstrate the successful dump of the status and contents of a specific block of CPU memory –Verify the FSW’s ability to cancel active memory dumps. NBTLMV – Narrowband Telemetry Verification –Verifies the successful transmission of housekeeping health and safety telemetry, alert telemetry, and diagnostic telemetry over the CTDB –Verifies the ability of the FSW to issue demand telemetry –Tests the bulk of the diagnostic telemetry issued by FSW –Verifies that FSW responds properly to valid housekeeping-related telecommands and low-rate science counter and thermal control FSW commands not covered in other test suites

September 16, 2005 FSW System Checkout TRR: Test Suites 7 Test Suites (6) OPMODE – Operational modes –Verify that FSW supports the observatory modes of (1) sky survey, (2) pointed observation, and (3) repointed observation, and supports the necessary commanded, autonomous, and GRB-driven transition among these observatory modes –Verify that FSW supports all required safety modes, and can correctly control the transition to LAT safe mode, correctly respond to load shedding messages from the spacecraft, and correctly manage entry into SAA and subsequent recovery from SAA –Confirms proper operation of the LAT in these observatory and safety modes, and proper reporting of mode changes in telemetry SIUCFG – Configuration of subsystems –Verify the ability of the SIU FSW to communicate with the LAT instrument subsystems for the purposes of configuration and retrieval of housekeeping and low rate science data (rate counters) –Verify the ability of FSW to configure the LAT power systems and the T&DF, TKR, CAL, and ACD subsystems as desired and read back the necessary configuration information to completely determine each subsystem’s configuration. –Verify that the FSW reports all configuration changes in telemetry

September 16, 2005 FSW System Checkout TRR: Test Suites 8 Test Suites (7) THRMCS – Thermal control system –Verify that the SIU FSW can properly execute the algorithms of the TCS implementation TIMPRC – Time signal processing –Verifies that the LAT FSW correctly processes the 1 Hz GPS “time hack” and the 1 Hz GPS time message from the spacecraft to provide a mapping of external time to the LAT internal 20 MHz clock, and that the resulting mapping allows event time measurements to be accurate to within 10 μsec of spacecraft time –Verifies that SIU FSW receives and records the GPS status information contained in the Ancillary Data message from the spacecraft VSGIFV – Vehicle Signals Interface Verification –Verifies the timing and processing of all discrete signals from the spacecraft –Verifies proper transitioning from primary to redundant signals

September 16, 2005 FSW System Checkout TRR: Test Suites 9 Test Suites (8) WBTLMV – Wideband telemetry verification –Verify the correct formatting and transmission of data through the external LAT science data interface in a format and sequence that may be correctly decoded –Confirm that data is delivered through the science data interface at the proper rate and within specified daily volume limits