Abstract:
                        
                        Positional covariances are required to do an assessment of collision probability, yet often such covariances are either not available or not typically provided. Spacecraft operators often receive a “black box” flight dynamics system which does not (or not readily) allow covariance matrices to be output, and even when allowed, it may be a covariance at the Orbit Determination (OD) epoch with either (1) no capability to provide a time history of covariance or (2) no capability to select the covariance reference frame, element set, units, timing system, or time step. Another example is the use of analytic or semi-analytic orbit propagators, which do not have a ready way to characterize or predict positional uncertainty. Yet another example is the provision of SSA services and information by military organizations that may be reluctant to share positional accuracy information from their system. Synthetic covariances offer a workaround for such cases, whereby positional precision (veracity or repeatability) can be taken as a minimum/lower bound measure of positional accuracy (absolute positional knowledge). In this paper, a review of approaches used to construct “synthetic covariances” from standard overlap comparisons is provided. In contrast to existing methods that assume the covariance matrix eigenvector reference frames or assume the functional dependence and suitability of error basis functions, we present a new digital statistics approach to 6x6 covariance uncertainty modeling that eliminates the need to assume a priori time-varying error functions for all error components and their correlations, with statistics drawn from within time and argument-of-latitude bins on an object-by-object basis. We compare the performance of this digital technique (and indeed the efficacy of using overlap tests as a proxy for covariance) with accuracies of Two-Line Elements (TLEs) and “Special Perturbations” high-accuracy numerically integrated ephemerides measured against well-solved “truth” reference orbits including calibration spheres, Wide Area Augmentation System (WAAS), and Global Navigation Satellite System (GNSS) satellites.
                        
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                                Oltrogge, D.L., Gist, R.G., Alfano, S., and Vallado, D.A., “Synthetic covariance production using a new digital approach,” IAA-ICSSA-24-16317, IAA Conference on SSA, Embry-Riddle University, Daytona Beach, FL, USA, 8 May 2024.