SU849839A1 - A METHOD FOR DETERMINING A GYRO ERROR FROM OVERLOADING - Google Patents

A METHOD FOR DETERMINING A GYRO ERROR FROM OVERLOADING

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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
Application number
SU2890743/23A
Other languages
Russian (ru)
Inventor
Г.И. Костенко
В.Н. Шеянов
Original Assignee
Г.И. Костенко
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Г.И. Костенко filed Critical Г.И. Костенко
Priority to SU2890743/23A priority Critical patent/SU849839A1/en
Application granted granted Critical
Publication of SU849839A1 publication Critical patent/SU849839A1/en

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  • 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.

SU2890743/23A 1980-03-03 1980-03-03 A METHOD FOR DETERMINING A GYRO ERROR FROM OVERLOADING SU849839A1 (en)

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)

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