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Realistic Covariance Prediction for the Earth Science ConstellationRoutine satellite operations for the Earth Science Constellation (ESC) include collision risk assessment between members of the constellation and other orbiting space objects. One component of the risk assessment process is computing the collision probability between two space objects. The collision probability is computed using Monte Carlo techniques as well as by numerically integrating relative state probability density functions. Each algorithm takes as inputs state vector and state vector uncertainty information for both objects. The state vector uncertainty information is expressed in terms of a covariance matrix. The collision probability computation is only as good as the inputs. Therefore, to obtain a collision calculation that is a useful decision-making metric, realistic covariance matrices must be used as inputs to the calculation. This paper describes the process used by the NASA/Goddard Space Flight Center's Earth Science Mission Operations Project to generate realistic covariance predictions for three of the Earth Science Constellation satellites: Aqua, Aura and Terra.
Document ID
20070017944
Document Type
Conference Paper
Authors
Duncan, Matthew (AI Solutions, Inc. Lanham, MD, United States)
Long, Anne (AI Solutions, Inc. Lanham, MD, United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2006
Subject Category
Space Sciences (General)
Meeting Information
AAS/AIAA Astrodynamics Specialist Conference(Keystone, CO)
Distribution Limits
Public
Copyright
Public Use Permitted.

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