Title :
An Application of Kalman Filtering and Time Averaging to Inertial Guidance Evaluation
Author :
Rosenthal, P.L. ; Brownlow, J.D.
Author_Institution :
Lockheed-California Company P.O. Box 551 D/72-51, B/310, P/B-6 Burbank, CA 91520
Abstract :
A method is developed for estimating circular error probable values and circular error probable rate values of an inertial navigation system using the concepts of Kalman filtering and time averaging.
Keywords :
Autocorrelation; Data analysis; Filtering; History; Inertial navigation; Kalman filters; Random variables; System performance; System testing; Target tracking;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.1985.310669
