DocumentCode :
1234815
Title :
Automatic on-line measurement of ship´s attitude by use of a servo-type accelerometer and inclinometers
Author :
Tanaka, Shogo ; Nishifuji, Seiji
Author_Institution :
Dept. of Electr. & Electron. Eng., Yamaguchi Univ., Ube, Japan
Volume :
45
Issue :
1
fYear :
1996
fDate :
2/1/1996 12:00:00 AM
Firstpage :
209
Lastpage :
217
Abstract :
For an accurate automatic on-line measurement of the ship´s attitude the paper develops an intelligent sensing system which uses one servo-type accelerometer and two servo-type inclinometers which are appropriately located on the ship. By considering the dynamics of the servo-controlled rigid pendulums of the inclinometers, linear observation equations are derived on the rolling and pitching signals of the ship. Moreover, one accelerometer is utilized to extract the heaving signal. Through the introduction of linear dynamic models and the linear observation equations for the three signals, their online measurement is reduced to the state estimation of the linear dynamic systems. A bank of Kalman filters is used to execute the on-line state estimation and to overcome changes in parameters in the dynamic models with time lapse
Keywords :
Kalman filters; accelerometers; attitude control; computerised instrumentation; intelligent sensors; pendulums; servomechanisms; ships; state estimation; Kalman filters; automatic online measurement; dynamic models; dynamics; heaving signal; inclinometers; intelligent sensing system; linear dynamic models; linear dynamic systems; linear observation equations; online state estimation; pitching signals; rolling; servo accelerometer; servo-controlled rigid pendulums; ship attitude; state estimation; Accelerometers; Costs; Equations; Gyroscopes; Intelligent systems; Marine vehicles; Sonar measurements; State estimation; Surface waves; Weight measurement;
fLanguage :
English
Journal_Title :
Instrumentation and Measurement, IEEE Transactions on
Publisher :
ieee
ISSN :
0018-9456
Type :
jour
DOI :
10.1109/19.481336
Filename :
481336
Link To Document :
بازگشت