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Analyzing the Relationship between Tracking and Covariance for Satellite Collision AvoidanceThis presentation will display statistical analysis performed with over 150,000 Conjunction Data Messages (CDMs) received for the Earth Observing System (EOS) Aqua, Aura and Terra satellites within the three year period of March 2015 through February 2018. The analysis performed demonstrates the relationship between the covariance of a secondary object and the amount of tracks it receives, as a function of Time to Closest Approach (TCA). The examination indicates that higher tracking frequencies result in lower uncertainties inclusively from the time the data is screened up until TCA. Further investigation displays the impacts of how additional observations of secondary objects lower their position uncertainties and what period of time prior to TCA convergence of the covariance can be expected depending on how well the objects are tracked. Data points from several recent EOS High Interest Events (HIEs) are used to exemplify this analysis.
Document ID
20180007758
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Hasan, Syed O.
(KBRwyle Greenbelt, MD, United States)
Date Acquired
November 19, 2018
Publication Date
November 13, 2018
Subject Category
Space Transportation And Safety
Space Communications, Spacecraft Communications, Command And Tracking
Report/Patent Number
GSFC-E-DAA-TN63119
Report Number: GSFC-E-DAA-TN63119
Meeting Information
Meeting: Space Situational Awareness (SSA) Operators'' Workshop 2018
Location: Denver, CO
Country: United States
Start Date: November 13, 2018
End Date: November 16, 2018
Sponsors: SpaceNav, LLC
Funding Number(s)
CONTRACT_GRANT: NNG17HP02C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Collision Avoidance
Orbital Debris
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