Research topic

Target Tracking and Data Fusion in Sensor Networks

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Research papers

1974 · IEEE Transactions on Automatic Control · 51,229 citations

A new look at the statistical model identification

The history of the development of statistical hypothesis testing in time series analysis is reviewed briefly and it is pointed out that the hypothesis testing procedure is not adequately defined as the procedure for statistical model identification. The classical maximum likelihood estimation procedure is reviewed and a new estimate minimum information theoretical criterion (AIC) estimate (MAICE) which is designed for the purpose of statistical identification is introduced. When there are several competing models the MAICE is defined by the model and the maximum likelihood estimates of the parameters which give the minimum of AIC defined by AIC = (-2)log-(maximum likelihood) + 2(number of independently adjusted parameters within the model). MAICE provides a versatile procedure for statistical model identification which is free from the ambiguities inherent in the application of conventional hypothesis testing procedure. The practical utility of MAICE in time series analysis is demonstrated with some numerical examples.

2011 · 13 citations

Helicopter Downwash/Frigate Airwake Interaction Flowfield PIV Surveys in a Low Speed Wind Tunnel

The work presented was performed at Old Dominion University and is part of a larger research program aimed at identifying interactions between rotor downwash and ship airwakes. The ODU Low-Speed Wind Tunnel was used with a simplified 1/50 scale frigate waterline model and traverse mounted powered rotor. Particle Image Velocimetry (PIV) velocity surveys were compared with rotor thrust coefficient measurements at locations of identified interaction to help understand the underlying flow physics. Initially, PIV surveys of the frigate model landing deck in isolation and the rotor in isolation were performed to provide a baseline flow understanding. A PIV flowfield survey was conducted with the ship in isolation, rotor in isolation and then the combined ship/rotor cases in order to compare superposed individual velocity fields to a combined measurement. Tests were performed with and without the presence of a rotary wing downwash influence on the landing deck centerline (y=0) for a wind-over-deck angle (WOD) of zero.