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Challenges Identifying Newly Launched Objects
Dr. T.S. Kelso
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Overview Background Preparing for Success Methodology
Tool Development & Validation Operational Performance Conclusions
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Background Large multi-payload deployments present unique SSA challenges Cubesat form factor & design make it even more so Need ways to quickly track & identify all payloads Failing to do so jeopardizes mission assurance & safety of flight
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Preparing for Success Operators can drive improvements
Pre-launch/post-deployment state vectors Share data in advance with JSpOC Develop independent tracking capability Two-way ranging GPS Simultaneous Doppler tracking Passive RFID techniques
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Methodology 4 cases involving Planet cubesats examined
2 prior to/2 following tool development Looking for key milestones Time to first TLE Time to unique identification Pre-Development Launch/Deployment Total Payloads Planet Payloads ISS (2016 May 16-Jun 2) 33 24 PSLV-C34 (2016 Jun 22) 20 12 Post-Development PSLV-C37 (2017 Feb 15) 104 88 KANOPUS-V-IK (2017 Jul 14) 73 48
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ISS Deployments (2016 May 16-Jun 2)
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PSLV-C34 Launch (2016 Jun 22)
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Tool Development Assignment/matching process Standard reporting
Based on RMS not closest distance Standard reporting Best match to operator data Best unique match to JSpOC data Multiple allowable matches to JSpOC data JSpOC objects having no matches Tool takes ~1 minute for 88-object case
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Tool Validation Two validation runs
All Planet TLEs against all JSpOC TLEs for Planet All matches correct—No Type I or Type II errors Correctly identified RapidEye as having no matches RMS values of 0.1 to 15.0 km All Planet TLEs against all ISS-related TLEs Correctly identified non-Planet objects as having no matches Best results for non-matches had RMS values in the thousands of kilometers
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Operational Performance
Results detailed on following slides PSLV-C37 demonstrated potential Required confidence building Found misidentification of INS-1B KANOPUS-V-IK showed dramatic improvement Significant delays for non-Planet objects Still working some identifications due to anomalies
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PSLV-C37 Launch (2017 Feb 15), Part 1
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PSLV-C37 Launch (2017 Feb 15), Part 2
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PSLV-C37 Launch (2017 Feb 15), Part 3
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KANOPUS-V-IK Launch (2017 Jul 14), Part 1
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KANOPUS-V-IK Launch (2017 Jul 14), Part 2
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Conclusions Significant improvement demonstrated
Having pre-launch vectors can help Identification requires independent tracking data and willingness to share Cubesat community needs to enable success Find/test solutions Seek ways to make available to all operators We must do better to support mission assurance & safety of flight
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Questions?
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