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Trending in Pc Measurements via a Bayesian Zero-Inflated Mixed ModelTwo satellites predicted to come within close proximity of one another, usually a high-value satellite and a piece of space debris moving the active satellite is a means of reducing collision risk but reduces satellite lifetime, perturbs satellite mission, and introduces its own risks. So important to get a good statement of the risk of collision in order to determine whether a maneuver is truly necessary. Two aspects of this Calculation of the Probability of Collision (Pc) based on the most recent set of position velocity and uncertainty data for both satellites. Examination of the changes in the Pc value as the event develops. Events should follow a canonical development (Pc vs time to closest approach (TCA)). Helpful to be able to guess where the present data point fits in the canonical development in order to guide operational response.
Document ID
20150019911
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Vallejo, Jonathon
(AI Solutions, Inc. Lanham, MD, United States)
Hejduk, Matthew
(Astrorum Consulting, LLC Waco, TX, United States)
Stamey, James
(Baylor Univ. Waco, TX, United States)
Date Acquired
October 29, 2015
Publication Date
October 19, 2015
Subject Category
Astrodynamics
Report/Patent Number
GSFC-E-DAA-TN26938
Report Number: GSFC-E-DAA-TN26938
Meeting Information
Meeting: International Symposium on Space Flight Dynamics
Location: Munich
Country: Germany
Start Date: October 19, 2015
End Date: October 23, 2015
Sponsors: Deutsches Zentrum fuer Luft- und Raumfahrt e.V.
Funding Number(s)
CONTRACT_GRANT: NNG14VC09C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Conjuction Assessment
Bayesian
Operations
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