DocumentCode :
1883202
Title :
Stability and stationarity in target kinematic modeling
Author :
Coraluppi, Stefano ; Carthel, Craig
Author_Institution :
Compunetix Inc., Monroeville, PA, USA
fYear :
2012
fDate :
3-10 March 2012
Firstpage :
1
Lastpage :
8
Abstract :
This paper analyzes a Mixed Ornstein-Uhlenbeck (MOU) process that has a number of appealing properties as a target motion model. Relevant earlier models that have been proposed include the standard nearly constant velocity motion model (unbounded long-term position and velocity), the Ornstein-Uhlenbeck process (bounded position, but no defined velocity), and the Integrated Ornstein-Uhlenbeck process (bounded velocity, but unbounded position). The Mixed Ornstein-Uhlenbeck (MOU) process exhibits drift terms in both position and velocity, and thus has a well-behaved limit for both. The initial target state can be defined in a natural way based on the steady-state characteristics of the MOU process, leading to a stationary stochastic process. Similarly, multi-target stationarity is achieved by choosing the initial target birth distribution according to the steady-state distribution on the number of targets. The MOU process can be used both in simulations and, correspondingly, in Kalman-based recursive filtering as part of multi-target tracking solutions.12
Keywords :
Kalman filters; recursive filters; stability; stochastic processes; target tracking; Kalman-based recursive filtering; integrated Ornstein-Uhlenbeck process; mixed Ornstein-Uhlenbeck process; multitarget stationarity; multitarget tracking; stability; standard nearly constant velocity motion model; stationary stochastic process; steady-state characteristics; target birth distribution; target kinematic modeling; target motion model; Computer aided software engineering; Covariance matrix; Filtering; Limiting; Process control; Steady-state; Tracking;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference, 2012 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
978-1-4577-0556-4
Type :
conf
DOI :
10.1109/AERO.2012.6187198
Filename :
6187198
Link To Document :
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