TY - GEN
T1 - Conjugate unscented transformation based orbital state estimation and sensor tasking for efficient space surveillance
AU - Adurthi, Nagavenkat
AU - Majji, Manoranjan
AU - Singla, Puneet
N1 - Copyright:
Copyright 2014 Elsevier B.V., All rights reserved.
PY - 2014
Y1 - 2014
N2 - This paper presents a novel sensor management framework to effectively monitor Resident Space Objects (RSOs) for Space Situational Awareness (SSA) applications. The central idea of the proposed methodology is to make use of information geometry for the characterization of current state of knowledge (situational awareness), which is used for the purpose of optimal sensor management. Recently developed Conjugate Unscented Transformation (CUT) method has been exploited to accurately and efficiently propagate non-Gaussian orbit state uncertainty and compute information metrics. Finally, an optimization problem is posed to solve for optimal sensing action while accounting for orbital state uncertainty. Numerical simulations are performed which illustrate the effectiveness of the proposed methodology in comparison to conventional methods which assume orbital density function to be Gaussian.
AB - This paper presents a novel sensor management framework to effectively monitor Resident Space Objects (RSOs) for Space Situational Awareness (SSA) applications. The central idea of the proposed methodology is to make use of information geometry for the characterization of current state of knowledge (situational awareness), which is used for the purpose of optimal sensor management. Recently developed Conjugate Unscented Transformation (CUT) method has been exploited to accurately and efficiently propagate non-Gaussian orbit state uncertainty and compute information metrics. Finally, an optimization problem is posed to solve for optimal sensing action while accounting for orbital state uncertainty. Numerical simulations are performed which illustrate the effectiveness of the proposed methodology in comparison to conventional methods which assume orbital density function to be Gaussian.
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M3 - Conference contribution
AN - SCOPUS:84906243272
SN - 9781624103087
T3 - AIAA/AAS Astrodynamics Specialist Conference 2014
BT - AIAA/AAS Astrodynamics Specialist Conference 2014
PB - American Institute of Aeronautics and Astronautics Inc.
T2 - AIAA/AAS Astrodynamics Specialist Conference 2014
Y2 - 4 August 2014 through 7 August 2014
ER -