DocumentCode
1366951
Title
Statistical Modeling of Rate Gyros
Author
Vaccaro, Richard J. ; Zaki, Ahmed S.
Author_Institution
Dept. of Electr., Comput., & Biomed. Eng., Univ. of Rhode Island, Kingston, RI, USA
Volume
61
Issue
3
fYear
2012
fDate
3/1/2012 12:00:00 AM
Firstpage
673
Lastpage
684
Abstract
Gyroscopes are integral components of inertial measurement units, which are used for guidance and stabilization of many platforms. This paper presents an algorithm for estimating the statistical parameters that govern the performance of rate gyros, i.e., the spectral densities R and Q of the angle random walk and rate random walk components, respectively. Previous work on gyro modeling is based on computing the Allan variance of a gyro signal and using a well-known formula for its mean. The algorithm in this paper uses these as well as the following quantities, which are derived in this paper: the theoretical variance of the Allan variance and the covariance between different Allan variance points. The algorithm is developed using the formulation of the best linear unbiased estimator from statistical estimation theory. The performance of the algorithm is demonstrated using simulated and experimental data. A bound on the error in the integral of the gyro output, as a function of Q and R, is also derived.
Keywords
aerospace instrumentation; covariance analysis; gyroscopes; Allan variance; angle random walk component; gyro modeling; gyroscope; inertial measurement unit; linear unbiased estimator; rate gyro signal; spectral density; statistical modeling; statistical parameter estimation theory; Calibration; Covariance matrix; Mathematical model; Noise; Random processes; Random variables; Vectors; Allan variance; best linear unbiased estimator; gyroscopes; inertial measurement units;
fLanguage
English
Journal_Title
Instrumentation and Measurement, IEEE Transactions on
Publisher
ieee
ISSN
0018-9456
Type
jour
DOI
10.1109/TIM.2011.2171609
Filename
6068252
Link To Document