NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Estimation With Range Dependent Sensor ModelThis paper focuses on the improvement of target tracking accuracy taking into account the sensor’s reading degradation as the relative range increases. The approach is based on the assumption that range measurement error depends on the actual range. Specifically, we model the measurement error as a proportional to the actual range term plus a zero-mean, Gaussian distributed, and uncorrelated process. We present two approaches to tracking a target with constant velocity model. The first approach uses Extended Kalman Filter (EKF) framework to estimate target's states and the unknown proportionality coefficient with linearization on the observation model on the predicted states at each time step. The second one uses a measurement conversion method to estimate the target's scaled by the unknown constant term states, which is shown to be unbiased. This conversion results in linear state and observation models, hence the standard Kalman filter can be applied. The actual target state is computed by application of back scaling with the estimate of unknown scale factor. We evaluate the approaches in desktop simulations.
Document ID
20210025810
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Vahram Stepanyan
(KBR (United States) Houston, Texas, United States)
Thomas Lombaerts
(KBR (United States) Houston, Texas, United States)
Chester V Dolph
(Langley Research Center Hampton, Virginia, United States)
Corey Ippolito
(Ames Research Center Mountain View, California, United States)
Date Acquired
December 10, 2021
Subject Category
Aerodynamics
Meeting Information
Meeting: AIAA SciTech Forum 2022
Location: San Diego, CA
Country: US
Start Date: January 3, 2022
End Date: January 7, 2022
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: 80ARC020D0010
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Technical Management
Keywords
Target tracking
sensor model
Kalman filter
No Preview Available