RU95107169A - Method of determination of natural drifts of three-axes gyroscopic stabilizer - Google Patents

Method of determination of natural drifts of three-axes gyroscopic stabilizer

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Publication number
RU95107169A
RU95107169A RU95107169/28A RU95107169A RU95107169A RU 95107169 A RU95107169 A RU 95107169A RU 95107169/28 A RU95107169/28 A RU 95107169/28A RU 95107169 A RU95107169 A RU 95107169A RU 95107169 A RU95107169 A RU 95107169A
Authority
RU
Russia
Prior art keywords
moment
axes
currents
correction
pulses
Prior art date
Application number
RU95107169/28A
Other languages
Russian (ru)
Inventor
В.И. Рыбаков
Original Assignee
В.И. Рыбаков
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 В.И. Рыбаков filed Critical В.И. Рыбаков
Priority to RU95107169/28A priority Critical patent/RU95107169A/en
Publication of RU95107169A publication Critical patent/RU95107169A/en

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  • Gyroscopes (AREA)

Abstract

FIELD: measurement technology. SUBSTANCE: invention is related to part of measurement technology which deals with problems of evaluation of gyroscopic devices and systems. Three-axes gyrostabilizer is set in advance by correction system to definite position relative to plane of horizon and meridian. Values of currents of correction of gyroscopes by three sensitive axes are measured and recorded in initial position. Alternating moments are formed by input axes of gyroscopes with the use of moment pickups. Amplitudes of first and second pulses of current have different values multiple of correction currents and polarity of first pulses of current is opposite to polarity of correction currents. Computations are carried out by formulas $$$; $$$, where H is kinetic moment of gyroscope: k is coefficient of transmission of moment pickup; $$$ are currents in moment pickup under action of first and second pulses of moment; $$$, are durations of first and second pulses of moment; $$$ is projection of angular speed on direction of input axis of gyroscope. EFFECT: reduced time of autonomous measurement of natural drifts of gyroscopic devices with preservation of accuracy. 1 cl, 2 dwg

Claims (1)

Изобретение относится к области измерительной техники, конкретно к той ее части, которая занимается вопросами оценки точности гироскопических приборов и систем. Позволяет сократить временные затраты автономного измерения собственных уходов гироскопических приборов при сохранении точности. Предварительно трехосный гиростабилизатор выставляется системой коррекции в определенное положение относительно плоскости горизонта и меридиана. В исходном положении измеряют и запоминают значения токов коррекции гироскопов по трем измерительным осям. По входным осям гироскопов при помощи датчиков момента формируются знакопеременные моменты, причем амплитуды первого и второго импульсов тока имеют различные величины, кратные значению токов коррекции, а полярность первых импульсов тока противоположна полярности токов коррекции. Вычисления выполняют по формулам, указанным в описании.The invention relates to the field of measuring equipment, specifically to that part of it, which deals with issues of assessing the accuracy of gyroscopic devices and systems. Allows you to reduce the time cost of autonomous measurement of their own departures of gyroscopic instruments while maintaining accuracy. Pre-triaxial gyrostabilizer is set by the correction system to a specific position relative to the horizon and meridian. In the initial position, the values of gyro correction currents are measured and stored along three measuring axes. Alternating moments are formed on the input axes of the gyroscopes with the help of torque sensors, the amplitudes of the first and second current pulses having different values that are multiples of the correction currents, and the polarity of the first current pulses is opposite to the polarity of the correction currents. The calculations are performed according to the formulas specified in the description.
RU95107169/28A 1995-05-04 1995-05-04 Method of determination of natural drifts of three-axes gyroscopic stabilizer RU95107169A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU95107169/28A RU95107169A (en) 1995-05-04 1995-05-04 Method of determination of natural drifts of three-axes gyroscopic stabilizer

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU95107169/28A RU95107169A (en) 1995-05-04 1995-05-04 Method of determination of natural drifts of three-axes gyroscopic stabilizer

Publications (1)

Publication Number Publication Date
RU95107169A true RU95107169A (en) 1996-12-20

Family

ID=48451105

Family Applications (1)

Application Number Title Priority Date Filing Date
RU95107169/28A RU95107169A (en) 1995-05-04 1995-05-04 Method of determination of natural drifts of three-axes gyroscopic stabilizer

Country Status (1)

Country Link
RU (1) RU95107169A (en)

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