DocumentCode
1006134
Title
The effect of gyro nonorthogonality error on gyrocompassing
Author
Priel, B.
Author_Institution
Israel Aircraft Ind., Yahud
Volume
28
Issue
3
fYear
1992
fDate
7/1/1992 12:00:00 AM
Firstpage
890
Lastpage
893
Abstract
The effect of the gyro nonorthogonality on the two-step gyrocompassing process is analyzed. It is shown that the azimuth misalignment resulting from gyro nonorthogonality depends on the platform direction with respect to geographic frame. Gyrocompassing error is explicitly expressed in terms of gyro nonorthogonality and gyro parameters. A compensation scheme to eliminate the gyrocompassing error, which results from gyro nonorthogonality, is presented. This method can be used in cases where the gyro nonorthogonality error is beyond the standard requirements for high quality platforms. The main advantage is that it allows an increase in the tolerance of gyro nonorthogonality, and reduces the cost of inertial measurement unit manufacture
Keywords
aircraft instrumentation; compensation; error correction; gyroscopes; inertial navigation; measurement errors; azimuth misalignment; compensation; gyro nonorthogonality error; gyrocompassing; inertial navigation; Accelerometers; Aircraft; Azimuth; Costs; Error correction; Manufacturing; Measurement standards; Measurement units; Navigation; Stability analysis;
fLanguage
English
Journal_Title
Aerospace and Electronic Systems, IEEE Transactions on
Publisher
ieee
ISSN
0018-9251
Type
jour
DOI
10.1109/7.256312
Filename
256312
Link To Document