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Assessment of the Gaussian Covariance Approximation over an Earth-Asteroid Encounter PeriodIn assessing the risk an asteroid may pose to the Earth, the asteroids state is often predicted for many years, often decades. Only by accounting for the asteroids initial state uncertainty can a measure of the risk be calculated. With the asteroids state uncertainty growing as a function of the initial velocity uncertainty, orbit velocity at the last state update, and the time from the last update to the epoch of interest, the asteroids position uncertainties can grow to many times the size of the Earth when propagated to the encounter risk corridor. This paper examines the merits of propagating the asteroids state covariance as an analytical matrix. The results of this study help to bound the efficacy of applying different metrics for assessing the risk an asteroid poses to the Earth. Additionally, this work identifies a criterion for when different covariance propagation methods are needed to continue predictions after an Earth-encounter period.
Document ID
20170005427
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Mattern, Daniel
(Omitron, Inc. Beltsville, MD, United States)
Date Acquired
June 9, 2017
Publication Date
June 1, 2017
Subject Category
Astrodynamics
Report/Patent Number
GSFC-E-DAA-TN42707
Report Number: GSFC-E-DAA-TN42707
Meeting Information
Meeting: International Symposium on Space Flight Dynamics (ISSFD) 2017
Location: Matsuyama
Country: Japan
Start Date: June 3, 2017
End Date: June 9, 2017
Sponsors: NASA Goddard Space Flight Center
Funding Number(s)
CONTRACT_GRANT: NNG14VC09C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
uncertainty characterization
Planetary defense
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