Multimodel filtering of partially observable space object trajectories

In this paper we present methods for multimodel filtering of space object states based on the theory of finite state time nonhomogeneous cadlag Markov processes and the filtering of partially observable space object trajectories. The state and observation equations of space objects are nonlinear and...

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Main Authors: Zatezalo, A., El-Fallah, A., Mahler, Ronald, Mehra, R., Pham, K.
Format: Conference Paper
Published: 2011
Online Access:http://hdl.handle.net/20.500.11937/56219
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author Zatezalo, A.
El-Fallah, A.
Mahler, Ronald
Mehra, R.
Pham, K.
author_facet Zatezalo, A.
El-Fallah, A.
Mahler, Ronald
Mehra, R.
Pham, K.
author_sort Zatezalo, A.
building Curtin Institutional Repository
collection Online Access
description In this paper we present methods for multimodel filtering of space object states based on the theory of finite state time nonhomogeneous cadlag Markov processes and the filtering of partially observable space object trajectories. The state and observation equations of space objects are nonlinear and therefore it is hard to estimate the conditional probability density of the space object trajectory states given EO/IR, radar or other nonlinear observations. Moreover, space object trajectories can suddenly change due to abrupt changes in the parameters affecting a perturbing force or due to unaccounted forces. Such trajectory changes can lead to the loss of existing tracks and may cause collisions with vital operating space objects such as weather or communication satellites. The presented estimation methods will aid in preventing the occurrence of such collisions and provide warnings for collision avoidance. © 2011 SPIE.
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spelling curtin-20.500.11937-562192017-09-13T16:11:24Z Multimodel filtering of partially observable space object trajectories Zatezalo, A. El-Fallah, A. Mahler, Ronald Mehra, R. Pham, K. In this paper we present methods for multimodel filtering of space object states based on the theory of finite state time nonhomogeneous cadlag Markov processes and the filtering of partially observable space object trajectories. The state and observation equations of space objects are nonlinear and therefore it is hard to estimate the conditional probability density of the space object trajectory states given EO/IR, radar or other nonlinear observations. Moreover, space object trajectories can suddenly change due to abrupt changes in the parameters affecting a perturbing force or due to unaccounted forces. Such trajectory changes can lead to the loss of existing tracks and may cause collisions with vital operating space objects such as weather or communication satellites. The presented estimation methods will aid in preventing the occurrence of such collisions and provide warnings for collision avoidance. © 2011 SPIE. 2011 Conference Paper http://hdl.handle.net/20.500.11937/56219 10.1117/12.884609 restricted
spellingShingle Zatezalo, A.
El-Fallah, A.
Mahler, Ronald
Mehra, R.
Pham, K.
Multimodel filtering of partially observable space object trajectories
title Multimodel filtering of partially observable space object trajectories
title_full Multimodel filtering of partially observable space object trajectories
title_fullStr Multimodel filtering of partially observable space object trajectories
title_full_unstemmed Multimodel filtering of partially observable space object trajectories
title_short Multimodel filtering of partially observable space object trajectories
title_sort multimodel filtering of partially observable space object trajectories
url http://hdl.handle.net/20.500.11937/56219