CLOSE APPROACH PREDICTION ANALYSIS OF THE EARTH SCIENCE CONSTELLATION WITH THE FENGYUN-1C DEBRIS Matthew Duncan - a.i. solutions, Inc. Colorado Springs, CO David Rand - a.i. solutions, Inc. Lanham, MD Goddard Space Flight Center Mission Operations and Mission Services/ Flight Dynamics Analysis Branch 14th Annual Improving Space Operations Workshop Suitland, Maryland April 15 - 16, 2008
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CLOSE APPROACH PREDICTION ANALYSIS OF THE EARTH SCIENCE CONSTELLATION WITH THE FENGYUN-1C DEBRIS Matthew Duncan - a.i. solutions, Inc. Colorado Springs,
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CLOSE APPROACH PREDICTION ANALYSIS OF THE EARTH SCIENCE CONSTELLATION
WITH THE FENGYUN-1C DEBRIS
Matthew Duncan - a.i. solutions, Inc. Colorado Springs, CODavid Rand - a.i. solutions, Inc. Lanham, MD
Goddard Space Flight Center Mission Operations and Mission Services/
Flight Dynamics Analysis Branch
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Agenda
► Overview and Goals
» Recent and Current Orbital Debris population
» Earth Science Constellation
» Earth Science Constellation and the Fengyun-1C Debris
► Long Term Prediction Method
» Easy High Performance Computing (HPC)
» Our solution in detail
» Process details
► Prediction Results
► Future Work
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2000 - Cataloged objects >10 cm diameter
Images courtesy NASA Orbital Debris Program Office
Recent Debris Population
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March 2007 - Tracked objects >10 cm diameter (FENGYUN-1C Debris in red)
Images courtesy NASA Orbital Debris Program Office
Current Debris Population
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► The collision risk due to orbital debris is increasing:» ~14,000 tracked objects >1 cm2
» Several hundred objects added to catalog each year (Ref. Liou & Johnson)► SFC Earth Observing assets reside in one of the most congested orbital regimes:
» Easy setup – more so than open source solutions; hours vs. days
» Integrates to existing network
Windows and HPC
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► Compute Cluster Server 2003
» Comfortably runs on inexpensive commodity hardware
» Relies on MS Active Directory network architecture
» Head node + several compute nodes
» Work submitted in a “job” made up of individual “tasks”
• A “task” is a single command line call to an executable
► FreeFlyer® mission analysis software
» GUI and command line interfaces
» Extensive database and file interface capabilities
» Native Windows application
► Extremely simple and easy to setup network topology
Our HPC Environment
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HeadNode CN01 CN02 CN03 CN04 CN05
Gigabit Switch
Corp. NetworkMonitor, Keyboard, Mouse on HeadNode
HPC Cluster Typical Configuration
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Problem: Using states of over 2200 objects, contained in a MySQL database, propagate each for 20 years and compare against ESC
Process:1. Create Representative ESC asset ephemeris data
» Three representative orbits (Aqua, Aura, Terra)2. Obtain states from database and build Ephemeris job template
» Each task is one 20 year propagation 3. Submit Ephemeris Generation template to cluster
» Propagate and record state data every 30 days» Drag modeled using Jacchia-Roberts with Schatten Mean-Nominal solar flux predictions + ballistic coefficient
4. Build compare template (2200 obj. x 3 ESC ≈ 6600 tasks)» Each task is comparison of one object and one asset ephemeris
5. Submit conjunction comparison template» Compare each pair every 30 days for 5 days and find conjunctions within 50 km sphere