SU849839A1 - A METHOD FOR DETERMINING A GYRO ERROR FROM OVERLOADING - Google Patents
A METHOD FOR DETERMINING A GYRO ERROR FROM OVERLOADINGInfo
- Publication number
- SU849839A1 SU849839A1 SU2890743/23A SU2890743A SU849839A1 SU 849839 A1 SU849839 A1 SU 849839A1 SU 2890743/23 A SU2890743/23 A SU 2890743/23A SU 2890743 A SU2890743 A SU 2890743A SU 849839 A1 SU849839 A1 SU 849839A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- overload
- gyroscope
- centrifuge
- rotation
- output signal
- Prior art date
Links
Landscapes
- Gyroscopes (AREA)
- Testing Of Engines (AREA)
Abstract
Способ определения ошибки гироскопа от перегрузки при испытании на центрифуге в режиме обратной связи по моменту, включающий установку гироскопа на центрифуге выходной осью параллельно оси вращения центрифуги, вращение ротора гиродвигателя, вращение центрифуги и измерение выходного сигнала гироскопа, отличающийся тем, что, с целью повышения точности, измерение выходного сигнала производят при двух скоростях вращения ротора гиродвигателя при наличии и отсутствии перегрузки, причем величину ошибки вычисляют по формуле:,где I - ошибка гироскопа от перегрузки;I, I- выходной сигнал гироскопа при двух значениях скорости и наличии перегрузки;I, I- выходной сигнал гироскопа при двух значениях скорости и отсутствии перегрузки;K - кратность скоростей.Method for determining gyroscope error from overload when tested on a centrifuge in the feedback mode on the moment, including the installation of a gyroscope on a centrifuge output axis parallel to the centrifuge axis of rotation, rotation of the gyro rotor, rotation of the centrifuge and measurement of the output signal of the gyroscope, characterized in that, to improve accuracy , the output signal is measured at two speeds of rotation of the rotor of the gyro engine in the presence and absence of overload, and the magnitude of the error is calculated by the formula:, where I is the error g roskop from overload; I, I - output signal of the gyroscope at two values of speed and the presence of overload; I, I - output signal of the gyroscope at two values of speed and no overload, K - multiplicity of speeds.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2890743/23A SU849839A1 (en) | 1980-03-03 | 1980-03-03 | A METHOD FOR DETERMINING A GYRO ERROR FROM OVERLOADING |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU2890743/23A SU849839A1 (en) | 1980-03-03 | 1980-03-03 | A METHOD FOR DETERMINING A GYRO ERROR FROM OVERLOADING |
Publications (1)
Publication Number | Publication Date |
---|---|
SU849839A1 true SU849839A1 (en) | 2005-08-20 |
Family
ID=60525146
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU2890743/23A SU849839A1 (en) | 1980-03-03 | 1980-03-03 | A METHOD FOR DETERMINING A GYRO ERROR FROM OVERLOADING |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU849839A1 (en) |
-
1980
- 1980-03-03 SU SU2890743/23A patent/SU849839A1/en active
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