Abstract
The work considers the results of the two-component micromechanical gyroscope error analysis. The simulator is created and its natural frequencies are defined as well. The mathematic simulation has been carried out and the elements influencing the precision of the gyroscope have been determined. The automatic frequency control algorithm is suggested and its efficiency is proved by computer testing.
| Original language | English |
|---|---|
| Title of host publication | Jubilee 15th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2008 - Proceedings |
| Publisher | State Research Center of the Russian Federation |
| Pages | 23-25 |
| Number of pages | 3 |
| ISBN (Print) | 9785900780801 |
| Publication status | Published - 2008 |
| Event | 15th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2008 - Saint Petersburg, Russian Federation Duration: 26 May 2008 → 28 May 2008 |
Other
| Other | 15th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2008 |
|---|---|
| Country | Russian Federation |
| City | Saint Petersburg |
| Period | 26.5.08 → 28.5.08 |
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Keywords
- Automatic frequency control algorithm
- Micromechanical gyroscope
- Natural frequencies
- Technological errors
ASJC Scopus subject areas
- Information Systems
- Signal Processing
- Computer Networks and Communications
- Electrical and Electronic Engineering
Cite this
Technological error analysis of the micromechanical gyroscope. / Lysova, O. M.; Nesterenko, T. G.; Plotnikova, I. V.
Jubilee 15th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2008 - Proceedings. State Research Center of the Russian Federation, 2008. p. 23-25.Research output: Chapter in Book/Report/Conference proceeding › Conference contribution
}
TY - GEN
T1 - Technological error analysis of the micromechanical gyroscope
AU - Lysova, O. M.
AU - Nesterenko, T. G.
AU - Plotnikova, I. V.
PY - 2008
Y1 - 2008
N2 - The work considers the results of the two-component micromechanical gyroscope error analysis. The simulator is created and its natural frequencies are defined as well. The mathematic simulation has been carried out and the elements influencing the precision of the gyroscope have been determined. The automatic frequency control algorithm is suggested and its efficiency is proved by computer testing.
AB - The work considers the results of the two-component micromechanical gyroscope error analysis. The simulator is created and its natural frequencies are defined as well. The mathematic simulation has been carried out and the elements influencing the precision of the gyroscope have been determined. The automatic frequency control algorithm is suggested and its efficiency is proved by computer testing.
KW - Automatic frequency control algorithm
KW - Micromechanical gyroscope
KW - Natural frequencies
KW - Technological errors
UR - http://www.scopus.com/inward/record.url?scp=84913595675&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84913595675&partnerID=8YFLogxK
M3 - Conference contribution
AN - SCOPUS:84913595675
SN - 9785900780801
SP - 23
EP - 25
BT - Jubilee 15th Saint Petersburg International Conference on Integrated Navigation Systems, ICINS 2008 - Proceedings
PB - State Research Center of the Russian Federation
ER -