Supernova/Acceleration Probe (SNAP) Mission/Science Operations Irene Bibyk Tim Rykowski Bob Schweiss June 28, 2001.

Slides:



Advertisements
Similar presentations
Questions from the European colleagues & Answers (only) from the Chinese engineers present for Y.-W. Zhang and S.-G. Yuan Chinese Academy of Space Technology.
Advertisements

PHEOS PSRR Concept of Operations. 2 Scope The purpose of the PCW-UVI Concept of Operations (ConOps) is to communicate how mission systems will operate,
Frank Stocklin Ron Vento Leslie Ambrose June 28,2001 SUPERNOVA/ACCELERATION PROBE (SNAP) Data Systems.
Automated File Transfer and Storage Management Concepts for Space Gary Meyers - GSFC Ed Criscuolo - CSC Keith Hogie - CSC Ron Parise - CSC Revised 6/14/2004.
Chapter 19: Network Management Business Data Communications, 4e.
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.
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 ProjectISOC Peer Review - March 2, 2004 Document: LAT-PR Section 2.1 Requirements 1 Gamma-ray Large Area Space Telescope GLAST Large.
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.
Page 1HMI Team Meeting – January 26, 2005 HMI Mission Operations Rock Bush HMI Stanford Program Manager Stanford University
JPL Autonomous Space Mission Simulation Flight Team Bob Hoffman Josh Ruggiero Adam Nikolic Dusty Terrill.
Secure System Administration & Certification DITSCAP Manual (Chapter 6) Phase 4 Post Accreditation Stephen I. Khan Ted Chapman University of Tulsa Department.
Mission Operations in Small Satellite Projects Making Mission Operations Effective J. Burkert Colorado Space Grant Consortium.
GLAST LAT ProjectISOC CDR, 4 August 2004 Document: LAT-PR-04500Section 21 GLAST Large Area Telescope: Instrument Science Operations Center CDR Section.
March 2004 At A Glance ITOS is a highly configurable low-cost control and monitoring system. Benefits Extreme low cost Database driven - ITOS software.
G O D D A R D S P A C E F L I G H T C E N T E R 1 The Trade Between CCSDS and HDLC Framing on Global Precipitation Measurement David Everett and Jonathan.
Marco Concha Charles Petruzzo June 28, 2001 SuperNova/ Acceleration Probe (SNAP) Flight Dynamics.
The Pursuit for Efficient S/C Design The Stanford Small Sat Challenge: –Learn system engineering processes –Design, build, test, and fly a CubeSat project.
Supernova/Acceleration Probe (SNAP) Reliability & System Safety Dick Bolt David Bogart June 28, 2001.
Bob G. Beaman June 28, 2001 Electrical Power System SuperNova / Acceleration Probe (SNAP)
Indian Ocean METOC Imager (IOMI) Operational Concept Demonstrates Military Operational Utility and Enables Improved Global Weather Prediction Data to Naval.
Open Source DTN for ISS Payloads Concept Proposal, 05-Jun Open-source DTN communication software for ISS Payloads Kevin K. Gifford BioServe Space.
1. 2 Purpose of This Presentation ◆ To explain how spacecraft can be virtualized by using a standard modeling method; ◆ To introduce the basic concept.
NASA’s Goddard Space Flight Center LRO Operations Concept Richard Saylor Jr. HTSI/Code 444 August 16-17, 2005.
MASSACHUSETTS INSTITUTE OF TECHNOLOGY NASA GODDARD SPACE FLIGHT CENTER ORBITAL SCIENCES CORPORATION NASA AMES RESEARCH CENTER SPACE TELESCOPE SCIENCE INSTITUTE.
20a - 1 NASA’s Goddard Space Flight Center Attitude Control System (ACS) Eric Holmes, Code 591 Joe Garrick, Code 595 Jim Simpson, Code 596 NASA/GSFC August.
Command and Data Handling (C&DH)
Aquarius Project Status 7 th Aquarius/SAC-D Science Team Meeting 11 April 2012.
Ground Support Network operations for the GRAS Radio Occultation Mission R. Zandbergen, the GRAS GSN team (ESOC) and the Metop GRAS team (EUMETSAT) 09/09/2011.
1 Lunar Reconnaissance Orbiter (LRO) CRaTER Technical Interchange Meeting C&DH Flight Software April 14, 2005.
CAPACITY Operational Atmospheric Chemistry Monitoring Missions CAPACITY Final Meeting - WP Ground Segment synthesis Final Meeting ESTEC02/06/05.
June 2004 SIW-4 - IP in Space Implementation Guide 1 Handbook for Using IP Protocols for Space Missions James Rash - NASA/GSFC Keith Hogie, Ed Criscuolo,
1 SpaceOps 2002 Autonomous Operations For The Swift Mission T3-47 John Ong/Swift Software Systems Manager NASA/GSFC Code 582/ Mike Rackley/Swift.
Page No. 1 Kelvin Nichols Payload Operations and Integration Center EO50 Delay Tolerant Networking (DTN) Implementation on the International Space Station.
.1 RESEARCH & TECHNOLOGY DEVELOPMENT CENTER SYSTEM AND INFORMATION SCIENCES JHU/MIT Proprietary Titan MESSENGER Autonomy Experiment.
THEMIS FDMO Review Management Topics − 1 October 5, 2004 Management Topics Manfred Bester.
Final Version Micro-Arcsecond Imaging Mission, Pathfinder (MAXIM-PF) Mission Operations Tim Rykowski Jeffrey Hosler May 13-17, 2002.
Section Number - 1 NASA’s Goddard Space Flight Center Communication Systems Jason A. Soloff NASA/GSFC Code 567 August 16-17, 2005.
Preparing for a Wind Lidar Venture Class Mission Discussion at Lidar Working Group Meeting Bar Harbor, ME August 24 – 26, 2010 Dr. Wayman Baker 1.
MWA Operations Management Plan (OMP, v. 3) Ron Remillard (MIT); MWA Project Meeting, June 6, 2011.
THEMIS FDMO CDR Peer Review − FOT Activities 1June 1-2, 2004 FOT Activities Mark Lewis.
DSL Distributed Systems Laboratory ATC 23 August Model Mission: Magnetospheric Multiscale (MMS) Mission Goal “To study the microphysics of three.
Space Operations as a Guide for a Real-World Scheduling Competition Eduardo Romero Marcelo Oglietti
GLAST Science Support CenterNovember, 2005 GSSC User Committee Meeting Tools for Mission and Observation Planning Robin Corbet, GSSC
TRIO-CINEMA Meeting at KHU 1 October 19-23, 2009 CINEMA Operations Manfred Bester.
Intelligent Distributed Spacecraft Infrastructure Earth Science Vision Session IGARSS 2002 Toronto, CA June 25, Needs for an Intelligent Distributed.
March 2004 At A Glance autoProducts is an automated flight dynamics product generation system. It provides a mission flight operations team with the capability.
NASA’s Goddard Space Flight Center Lunar Reconnaissance Orbiter Ground System Requirements.
Telemetry Constraints during Early Operations The STEREO telemetry rate is restricted during the phasing orbits due to S/C RF interference with each other,
Solar Probe Plus A NASA Mission to Touch the Sun March 2015 Instrument Suite Name Presenter's Name.
Aquarius Mission Simulation A realistic simulation is essential for mission readiness preparations This requires the ability to produce realistic data,
Final Version Kequan Luu May 13-17, 2002 Micro-Arcsecond Imaging Mission, Pathfinder (MAXIM-PF) Flight Software.
Science Operation Readiness Review ICESat SIPS (I-SIPS) Status N0v 30, 2001 David Hancock ICESat Science Ground System Manager
John Martin April 5, 2001 SuperNova/ Acceleration Probe (SNAP) Introduction.
1. 2 Purpose of This Presentation ◆ To explain how spacecraft can be virtualized by using a standard modeling method; ◆ To introduce the basic concept.
Tracing the JWST Proposal from User Interface to Commanding of an Instrument Margaret Meixner & WIT Balzano, Robinson & CMD.
SRR and PDR Charter & Review Team Linda Pacini (GSFC) Review Chair.
Requirements to WSO Ground Segment Lavochkin Association & ROSCOSMOS 30/06/2006.
March 2004 At A Glance ITPS is a flexible and complete trending and plotting solution which provides user access to an entire mission full-resolution spacecraft.
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.
ESA UNCLASSIFIED – For Official Use HSO-OP - Solar and Planetary Missions Division Solar Orbiter Instrument Operations, Data Handling and FDIR Ignacio.
March 2004 At A Glance The AutoFDS provides a web- based interface to acquire, generate, and distribute products, using the GMSEC Reference Architecture.
EIS Operation Planning H. Hara (NAOJ) 2007 Dec 10.
Terry Smith June 28, 2001 Command and Data Handling System SuperNova / Acceleration Probe (SNAP)
GLAST Large Area Telescope:
SDO Flight Dynamics Subsystem
Launch and On-orbit Checkout
Technology for a NASA Space-based Science Operations Grid Internet2 Members Meeting Advanced Applications Track Session April, 2003 Robert N. Bradford.
ZERO LATENCY Satellite Data Delivery DEMAND AND CHALLENGES
Presentation transcript:

Supernova/Acceleration Probe (SNAP) Mission/Science Operations Irene Bibyk Tim Rykowski Bob Schweiss June 28, 2001

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 2 Mission/Science Operations Topics  Recommended Implementation Approach  Recommended Operations Staffing Approach  Critical Requirements and Assumptions  Cost Summary  Options Presented  Basis of Estimate  Additional Trades to Consider  Risk Assessment  Issues and Concerns  Back-up Slides

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 3 Mission/Science Operations Recommended Development Approach  Use Berkeley SSL MOC as basis for SNAP MOC development  Will meet all operational requirements for SNAP operations  Proven system operationally (FAST support, will support HESSI)  Includes basic functionality, plus automation tools to support SNAP operations in an 8x5 manner  Use NERSC at Berkeley for L0 and higher level data processing  Significant storage and computing resources currently available  Potential modifications to this system were not considered as part of this study and may need to be investigated  Minimal modifications will be required to Berkeley SSL MOC to support SNAP operations  Some hardware upgrades are necessary (additional dedicated string for SNAP R/T support, additional general purpose workstations, network hardware)  SNAP software-specific modifications, primarily to support  Flight dynamics operations (I.e., lunar flyby) during commissioning  Command management  Mission/Science planning and scheduling

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 4 Mission/Science Operations Recommended Operations Staffing Approach  Recommend 8x5 (weekday, prime shift) staffing profile for routine mission operations  Most cost-effective solution for SNAP Mission Operations  Appropriate for both 3 and 5 ground station option  Scheduling complexity not much different between two options  Relatively simple mission operations concept allows 8x5 operations approach to be pursued:  Minimal instrument planning and scheduling (target observations uplinked once every 4 days)  No orbit maneuvers beyond commissioning phase  Minimal recovery operations conducted for data lost or not available  Spectroscopy and spacecraft housekeeping data stored on-board, replay from storage can be automated and accommodated in nominal 55 Mbps downlink  No attempts to store/recover other data lost due to link problems, gaps in station coverage

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 5 Mission/Science Operations Critical Requirements and Assumptions  Data rates:  Average SNAP instrument data rate: ~52 Mbps  Includes lossless compression plus CCSDS overhead  Average SNAP HK data rate: 16 kbps  Data Latency:  ~4 days latency to deliver raw instrument data to NERSC is acceptable.  Space-Ground contact profile  One 8 hour contact per day at each of three sites (Berkeley, France, Japan)  Some gaps in coverage expected, gaps would be reduced by optional use of Hawaii, Santiago stations  MOC functionality:  MOC provides “standard” set of functionality to support Mission Operations (e.g., S/C and instrument commanding,mission planning/scheduling, RT TLM monitoring, offline analysis,  Facilities/Resources available:  Berkeley SSL MOC used for Mission Operations  NERSC used for Level zero/higher level science data processing  Sufficient communications bandwidth available at no cost to SNAP from both France and Japan ground station sites  ~10 Mbps communications capability required from each remote ground site to Berkeley to satisfy latency requirements

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 6 Mission/Science Operations Cost Basis of Estimate  Mission Operations Cost Assumptions  Existing Berkeley SSL MOC serves as development basis  One additional equipment string costed for real-time support  Existing equipment strings can be used to provide hot backups, off- line test/maintenance function  Years costed for software development  Primarily to tailor existing Berkeley SSL MOC system to support SNAP mission  Bandwidth from France, Japan stations available at no cost to SNAP  No additional costs for Level 0/Science data processing (assume use of NERSC system)  Operations Staffing Cost Assumptions  First year (L-30 mos. to L-18 mos.): 1.8 heads for ops planning activities  Second year (L-18 mos. To L-6 mos.): 5.2 heads for development/test of ops products and plans  L-6 mos. to L+3: 9.5 heads for pre-launch ops rehearsals/sims, launch support, early orbit checkout, etc.  Nominal (6.3 heads) staffing level reached at L+12

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 7 Mission/Science Operations Additional Trades to Consider  3 ground stations option  Add capability to store on-board full SNAP science bandwidth during gaps in coverage, with later downlink  (+) Increases percentage of data recovery  (-) Increases costs for C&DH and Mission Operations as a minimum.

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 8 Mission/Science Operations Risk Assessment  No risks identified

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 9 Mission/Science Operations Issues and Concerns  No issues or concerns

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 10 Mission/Science Operations Backup Charts

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 11 Mission/Science Operations Driving Mission Characteristics  Launch: October 2008  Mission lifetime: Nominal mission duration 2 years, with 5 year goal  Orbit overview: 19x57 Re  Space-Ground contacts:  3 ground station option: 3 station contacts per day at Northern Latitude ground stations (Berkeley CA, Lyon France, Japan)  Data rates:  Average instrument data rate: 52 Mbps aggregate (assumes lossless compression and overhead)  Engineering/HK: 16 kbps (assumed )

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 12 Mission/Science Operations Driving Mission Characteristics (cont.)  Spacecraft summary:  CCSDS compliant  24 hours of on-board data storage for spectrometer and engineering data  Operations summary:  No orbit adjustments necessary after commissioning  Well defined instrument observations  Sequence of targets uplinked to spacecraft every 4 days  No target of opportunity observations envisioned.  Majority of commanding is preplanned and is needed no more than once per day.  Latency requirements:  4 days to deliver raw telemetry from ground stations to NERSC for Level 0 and higher level data processing

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 13  Support operations of SNAP satellite  Processing/display of real-time telemetry and status data  Spacecraft and instrument commanding  Attitude determination and orbit analysis  HK Dump data receipt and processing for contingency  Ground Station (GS) scheduling  Engineering data analysis  Interact with ground station for satellite communications  Telemetry, command and status data  Electronic transfer of data to MOC/NERSC during each contact  Station scheduling  Voice communications Mission Operations Driving Requirements

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 14 Mission Operations Driving Requirements (cont.)  Level 0 processing provided by National Energy Research and Scientific Computing Center (NERSC)  Architecture for Level 0 processing not provided or costed for this mission  Provide automation to facilitate reduced operations staffing, to include “lights-out” operations on weekday off-shifts and weekends  Automatically recognize alarm conditions and notify remote operations personnel during unstaffed operations  Automatically handle receipt of data dumps from GS’s and generation/delivery of Level 0 data products

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 15 Mission Operations Assumptions  “Lights-Out” operations approach acceptable for normal operations to minimize operations costs  Satellite can nominally operate for up to 3 days without ground contact  Spacecraft and instruments autonomously manage health-and- safety (i.e., they will detect problems and safe themselves when necessary)  Typical Real-Time System Reliability, Maintainability, and Availability (RMA) is required  Hot backups needed for critical telemetry and command processors and provided as part of “infrastructure” available at Berkeley Space Science Laboratory (SSL)  Typical command constraint checking is sufficient  Minimal planning and scheduling needed given simplicity of spacecraft and instrument operations

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 16 Mission Operations Technologies Required  MOC must be able to support the automated handling of specific functions/activities  Automatically process real-time data (housekeeping and science)  Automatically monitor telemetry, recognize error/alarm conditions, and notify offsite operations staff  Provide remote offsite operations personnel with remote access to data without violating security requirements  Automatically perform engineering analysis on housekeeping data  Generate trend plots, statistics reports, etc. for FOT analysis  Recognize error/alarm conditions and notify remote operations personnel  Berkeley SSL MOC contains all required technologies

SNAP, June 25-28, 2001 Goddard Space Flight Center Mission/Science Operations Page 17 Mission/Science Operations Subsystem Summary  Technology Readiness Level: 8-9 (all required technologies have been at least demonstrated, most in currently operational systems)  Space-GND contacts: nominally 3 per day of 8 hours each at Northern Latitude ground stations (Berkeley, France, Japan)  Avg Aggregate Instrument Data Rate: ~52 Mbps (includes lossless compression plus overhead)  Planning and Scheduling Requirements: Minimal  Science Data Processing Requirements: Delivery science data to NERSC from ground stations with no more than 4 day latency  Technology Complexity: Minimal, currently available/operational technology proposed  Risk: Minimal