DocumentCode :
1302351
Title :
Geolocation of a known altitude object from TDOA and FDOA measurements
Author :
Ho, K.C. ; Chan, Y.T.
Author_Institution :
Dept. of Electr. Eng., Saskatchewan Univ., Saskatoon, Sask., Canada
Volume :
33
Issue :
3
fYear :
1997
fDate :
7/1/1997 12:00:00 AM
Firstpage :
770
Lastpage :
783
Abstract :
Most satellite systems for locating an object on Earth use only time difference of arrival (TDOA) measurements. When there are relative motions between an emitter and receivers, frequency difference of arrival (FDOA) measurements can be used as well. Often, the altitude of an object is known (it is zero, for example) or can be measured with an altimeter. Two sets of geolocation solutions are proposed which exploit the altitude constraint to improve the localization accuracy. One is for TDOAs alone and the other for the combination of TDOA and FDOA measurements. The additional complexity by imposing the constraint is a one-dimensional Newton´s search and the rooting of a polynomial. The covariance matrices of the new estimators are derived under a small measurement noise assumption and shown to attain the constrained Cramer-Rao lower bound (CRLB). When there is a bias error in the assumed altitude, using the altitude constraint will introduce a bias to the solution. Since applying the constraint decreases the variance, there is a tradeoff between variance and bias in the mean square error (MSE). The maximum allowable altitude error such that the constraint solution will remain superior to the unconstraint is given. Simulation results are included to corroborate the theoretical development.
Keywords :
Newton method; covariance matrices; direction-of-arrival estimation; object detection; polynomials; satellite navigation; signal detection; altitude constraint; bias error; constrained Cramer-Rao lower bound; covariance matrices; frequency difference of arrival measurements; geolocation solutions; known altitude object geolocation; localization accuracy; maximum allowable altitude error; mean square error; oblate spheroid model; one-dimensional Newton´s search; polynomial rooting; relative emitter-receiver motions; satellite systems; small measurement noise assumption; time difference of arrival measurements; Covariance matrix; Earth; Frequency measurement; Global Positioning System; Military computing; Military satellites; Polynomials; Position measurement; Sea measurements; Time difference of arrival; Time measurement;
fLanguage :
English
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9251
Type :
jour
DOI :
10.1109/7.599239
Filename :
599239
Link To Document :
بازگشت