SU1619850A1 - METHOD FOR DETERMINING THE PERFECTION OF THE PERFORMANCE OF THE AXIS SENSOR OF THE ANGLE OF A DYNAMICALLY ADJUSTABLE GYROSCOPE WITH THE PERIPENDICULARITY OF THE AXES OF THE SENSOR OF THE SENSOR - Google Patents
METHOD FOR DETERMINING THE PERFECTION OF THE PERFORMANCE OF THE AXIS SENSOR OF THE ANGLE OF A DYNAMICALLY ADJUSTABLE GYROSCOPE WITH THE PERIPENDICULARITY OF THE AXES OF THE SENSOR OF THE SENSORInfo
- Publication number
- SU1619850A1 SU1619850A1 SU4631338/22A SU4631338A SU1619850A1 SU 1619850 A1 SU1619850 A1 SU 1619850A1 SU 4631338/22 A SU4631338/22 A SU 4631338/22A SU 4631338 A SU4631338 A SU 4631338A SU 1619850 A1 SU1619850 A1 SU 1619850A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- sensor
- axes
- angle
- determining
- perpendicularity
- Prior art date
Links
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- Gyroscopes (AREA)
Abstract
Способ определения неперпендикулярности осей датчика угла динамически настраиваемого гироскопа при наличии перпендикулярности осей датчика момента, включающий последовательное введение постоянного смещения в каждый из каналов коррекции и измерение изменений токов в датчиках момента, отличающийся тем, что, с целью повышения его точности, измерение изменений токов в датчиках момента производят при двух направлениях вращения ротора гироскопа, а неперпендикулярность δψ осей датчика угла определяют по формуламδψ = ψ+ ψ;где ψ, ψ- угол между осями датчика угла и датчика момента, установленными на одной оси;ΔI, ΔI- изменение тока в моментном датчике соответствующего канала коррекции, причем один штрих соответствует прямому направлению вращения ротора, а два штриха - обратному;K, K- крутизна по току датчиков момента соответствующих каналов коррекции.The method for determining the non-perpendicularity of the axes of the angle sensor of a dynamically tuned gyroscope in the presence of perpendicularity of the axes of the torque sensor, including the sequential introduction of a constant offset into each of the correction channels and the measurement of changes in currents in torque sensors, characterized in that, in order to increase its accuracy, measurement of changes in currents in sensors moment is produced at two directions of rotation of the gyroscope rotor, and non-perpendicularity δψ of the axes of the angle sensor is determined by the formulas δ = ψ + ψ, where ψ, ψ are the angle between the axes of the angle sensor and the torque sensor installed on the same axis; ΔI, ΔI is the current change in the torque sensor of the corresponding correction channel, with one stroke corresponding to the forward direction of rotation of the rotor, and two bars to the reverse; K, K is the slope of the current torque sensors channel correction.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4631338/22A SU1619850A1 (en) | 1989-01-04 | 1989-01-04 | METHOD FOR DETERMINING THE PERFECTION OF THE PERFORMANCE OF THE AXIS SENSOR OF THE ANGLE OF A DYNAMICALLY ADJUSTABLE GYROSCOPE WITH THE PERIPENDICULARITY OF THE AXES OF THE SENSOR OF THE SENSOR |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4631338/22A SU1619850A1 (en) | 1989-01-04 | 1989-01-04 | METHOD FOR DETERMINING THE PERFECTION OF THE PERFORMANCE OF THE AXIS SENSOR OF THE ANGLE OF A DYNAMICALLY ADJUSTABLE GYROSCOPE WITH THE PERIPENDICULARITY OF THE AXES OF THE SENSOR OF THE SENSOR |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1619850A1 true SU1619850A1 (en) | 2005-07-20 |
Family
ID=60520030
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU4631338/22A SU1619850A1 (en) | 1989-01-04 | 1989-01-04 | METHOD FOR DETERMINING THE PERFECTION OF THE PERFORMANCE OF THE AXIS SENSOR OF THE ANGLE OF A DYNAMICALLY ADJUSTABLE GYROSCOPE WITH THE PERIPENDICULARITY OF THE AXES OF THE SENSOR OF THE SENSOR |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1619850A1 (en) |
-
1989
- 1989-01-04 SU SU4631338/22A patent/SU1619850A1/en active
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