Abstract
The analytic gyrocompass system (AGS) consists of three or two single-axis accelerometers, two components rate gyro based on dynamically turned gyro (DTG) and computer. This type of AGS is the base of gyro inclinometer. Inclinometer exploitation showed reducing of the precision of determination of orientation parameters during time. The main reasons are mechanical actions on hole probe. The blows create the appearance of residual deformation of DTG joint flexure assembly. The authors ascertained the dependence of rate gyro error from device orientation relatively to gravity vector. The error model of rate gyro was received. Eight constants, that are members of the expression for calculation of corrected angular rates values are defined during conducting of the recurrent metrological calibration test. It is necessary to know the values of angular rate measured by device in its eight different attitude relatively geographic oriented coordinate system. For realization of offered method it is necessary to have two axis test stand. The expressions for calculation of corrected angular rates, the formulas for determination constants of this expressions and the requirements of the stand are given. Experimental tests of this method have shown that error of definition orientation in azimuth AGS, based on DTG like GVK-6, that have been used earlier in hole device inclinometer composition have reduced more than one order (from 3-4 degree to 0.1-0.2).
| Original language | English |
|---|---|
| Title of host publication | 5th Korea-Russia International Symposium on Science and Technology - Proceedings |
| Subtitle of host publication | KORUS 2001 |
| Publisher | Institute of Electrical and Electronics Engineers Inc. |
| Pages | 26-29 |
| Number of pages | 4 |
| Volume | 1 |
| ISBN (Electronic) | 0780370082, 9780780370081 |
| DOIs | |
| Publication status | Published - 2001 |
| Event | 5th Korea-Russia International Symposium on Science and Technology, KORUS 2001 - Tomsk, Russian Federation Duration: 26 Jun 2001 → 3 Jul 2001 |
Conference
| Conference | 5th Korea-Russia International Symposium on Science and Technology, KORUS 2001 |
|---|---|
| Country | Russian Federation |
| City | Tomsk |
| Period | 26.6.01 → 3.7.01 |
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Keywords
- analytic gyrocompass system
- automation
- calibration
- compensation
- dynamically turned gyro
- error
- stand
ASJC Scopus subject areas
- Clinical Biochemistry
- Computer Networks and Communications
- Biotechnology
- Civil and Structural Engineering
- Mechanics of Materials
- Electronic, Optical and Magnetic Materials
- Materials Chemistry
- Surfaces, Coatings and Films
Cite this
The increase of analytic gyrocompass system precision constructed on dynamically turned gyro. / Belyanin, L. N.; Golikov, A. N.; Martemyanov, V. M.
5th Korea-Russia International Symposium on Science and Technology - Proceedings: KORUS 2001. Vol. 1 Institute of Electrical and Electronics Engineers Inc., 2001. p. 26-29 975044.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - The increase of analytic gyrocompass system precision constructed on dynamically turned gyro
AU - Belyanin, L. N.
AU - Golikov, A. N.
AU - Martemyanov, V. M.
PY - 2001
Y1 - 2001
N2 - The analytic gyrocompass system (AGS) consists of three or two single-axis accelerometers, two components rate gyro based on dynamically turned gyro (DTG) and computer. This type of AGS is the base of gyro inclinometer. Inclinometer exploitation showed reducing of the precision of determination of orientation parameters during time. The main reasons are mechanical actions on hole probe. The blows create the appearance of residual deformation of DTG joint flexure assembly. The authors ascertained the dependence of rate gyro error from device orientation relatively to gravity vector. The error model of rate gyro was received. Eight constants, that are members of the expression for calculation of corrected angular rates values are defined during conducting of the recurrent metrological calibration test. It is necessary to know the values of angular rate measured by device in its eight different attitude relatively geographic oriented coordinate system. For realization of offered method it is necessary to have two axis test stand. The expressions for calculation of corrected angular rates, the formulas for determination constants of this expressions and the requirements of the stand are given. Experimental tests of this method have shown that error of definition orientation in azimuth AGS, based on DTG like GVK-6, that have been used earlier in hole device inclinometer composition have reduced more than one order (from 3-4 degree to 0.1-0.2).
AB - The analytic gyrocompass system (AGS) consists of three or two single-axis accelerometers, two components rate gyro based on dynamically turned gyro (DTG) and computer. This type of AGS is the base of gyro inclinometer. Inclinometer exploitation showed reducing of the precision of determination of orientation parameters during time. The main reasons are mechanical actions on hole probe. The blows create the appearance of residual deformation of DTG joint flexure assembly. The authors ascertained the dependence of rate gyro error from device orientation relatively to gravity vector. The error model of rate gyro was received. Eight constants, that are members of the expression for calculation of corrected angular rates values are defined during conducting of the recurrent metrological calibration test. It is necessary to know the values of angular rate measured by device in its eight different attitude relatively geographic oriented coordinate system. For realization of offered method it is necessary to have two axis test stand. The expressions for calculation of corrected angular rates, the formulas for determination constants of this expressions and the requirements of the stand are given. Experimental tests of this method have shown that error of definition orientation in azimuth AGS, based on DTG like GVK-6, that have been used earlier in hole device inclinometer composition have reduced more than one order (from 3-4 degree to 0.1-0.2).
KW - analytic gyrocompass system
KW - automation
KW - calibration
KW - compensation
KW - dynamically turned gyro
KW - error
KW - stand
UR - http://www.scopus.com/inward/record.url?scp=84961771246&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84961771246&partnerID=8YFLogxK
U2 - 10.1109/KORUS.2001.975044
DO - 10.1109/KORUS.2001.975044
M3 - Conference contribution
AN - SCOPUS:84961771246
VL - 1
SP - 26
EP - 29
BT - 5th Korea-Russia International Symposium on Science and Technology - Proceedings
PB - Institute of Electrical and Electronics Engineers Inc.
ER -