Collision avoidance relies on representative Cartesian uncertainty volumes in order to calculate probabilities of collision. Among the potential shortcomings of a covariance matrix representation of state errors, the most worrisome is the coordinate mismatch between the Cartesian framework in which these matrices are distributed and the curvilinear path that satellite orbits actually follow. The present study compares curvilinear-based and Cartesian covariance representations for ~50,000 conjunctions to determine the frequency in which significant deviations from Gaussianity are observed, then compares the 2-D Pc result from the Cartesian covariance to a Monte Carlo Pc conducted in element space to assess operational significance
This presentation applies a covariance realism technique to the National Aeronautics and Space Admin...
A covariance realism process for NASA's Global Precipitation Measurement (GPM) spacecraft is detaile...
Probability of collision (P(sub c)) estimates for Earth-orbiting satellites typically assume a tempo...
Collision avoidance relies on representative Cartesian uncertainty volumes in order to calculate pro...
The NASA Conjunction Assessment Risk Analysis team estimates the probability of collision (Pc) for a...
The purpose of covariance realism is to properly size a primary object's covariance in order to add ...
The manipulation of space object covariances to try to provide additional or improved information to...
Primary and secondary covariances combined and projected into conjunction plane (plane perpendicular...
Satellite conjunction risk typically evaluated through the probability of collision (Pc). Considers ...
Two satellites predicted to come within close proximity of one another, usually a high-value satelli...
In order to calculate operationally accurate collision probabilities, the position error covariance ...
The NASA Conjunction Assessment Risk Analysis team has implemented new software to estimate the prob...
A simple model is proposed to predict the behavior of Probabilities of Collision (P(sub c)) for conj...
While the two-dimensional probability of collision (Pc) calculation has served as the main input to ...
Probability of collision (P(sub c)) estimates for Earth-orbiting satellites typically assume a tempo...
This presentation applies a covariance realism technique to the National Aeronautics and Space Admin...
A covariance realism process for NASA's Global Precipitation Measurement (GPM) spacecraft is detaile...
Probability of collision (P(sub c)) estimates for Earth-orbiting satellites typically assume a tempo...
Collision avoidance relies on representative Cartesian uncertainty volumes in order to calculate pro...
The NASA Conjunction Assessment Risk Analysis team estimates the probability of collision (Pc) for a...
The purpose of covariance realism is to properly size a primary object's covariance in order to add ...
The manipulation of space object covariances to try to provide additional or improved information to...
Primary and secondary covariances combined and projected into conjunction plane (plane perpendicular...
Satellite conjunction risk typically evaluated through the probability of collision (Pc). Considers ...
Two satellites predicted to come within close proximity of one another, usually a high-value satelli...
In order to calculate operationally accurate collision probabilities, the position error covariance ...
The NASA Conjunction Assessment Risk Analysis team has implemented new software to estimate the prob...
A simple model is proposed to predict the behavior of Probabilities of Collision (P(sub c)) for conj...
While the two-dimensional probability of collision (Pc) calculation has served as the main input to ...
Probability of collision (P(sub c)) estimates for Earth-orbiting satellites typically assume a tempo...
This presentation applies a covariance realism technique to the National Aeronautics and Space Admin...
A covariance realism process for NASA's Global Precipitation Measurement (GPM) spacecraft is detaile...
Probability of collision (P(sub c)) estimates for Earth-orbiting satellites typically assume a tempo...