FIELD: physics, measurement technology.
SUBSTANCE: invention relates to gryscope instrument-making and is meant for determining scaling factors of a laser gyroscope when performing calibration (certification) of strap down inertial navigation systems. The method of determining scaling factors of a laser gyroscope comprises mounting a laser gyroscope on the face plate of a rotary table, further successively turning the face plate in opposite directions by a fixed angle αT, wherein at the output of the laser gyroscope for its sensitivity axis, the number of information symbols and their sign are recorded, wherein the turns of the face plate by an angle αT are performed successively relative to three orthogonal axes of rotation OX, OY, OZ, with each sensitivity axis of the laser gyroscope making a complete turn by an angle αT, then determining the scaling factor Ki of the corresponding sensitivity axis of the laser gyroscope from the relationship: where i=1, 2, … is the number of the sensitivity axis of the laser gyroscope; is the half-difference between the number of information pulses, detected for the i-th sensitivity axis of the laser gyroscope during successive turns of the face plate in opposite directions by an angle αT relative to the axis of rotation OX; is the half-difference between the number of information pulses detected for the i-th sensitivity axis of the laser gyroscope during successive turns of the face plate in opposite directions by an angle αT relative to the axis of rotation OY; is the half-difference between the number of information pulses detected for the i-th sensitivity axis of the laser gyroscope during successive turns of the face plate in opposite directions by an angle αT relative to the axis of rotation OZ.
EFFECT: invention increases the accuracy of determining scaling factors of a laser gyroscope and broadens functional capabilities.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF DETERMINING SCALING FACTORS OF TRIAXIAL LASER GYROSCOPE | 2015 |
|
RU2599182C1 |
METHOD OF DETERMINING NON-ORTHOGONALITY OF SENSITIVITY AXES OF LASER GYROSCOPE | 2019 |
|
RU2727318C1 |
METHOD OF DETERMINING SYSTEMATIC COMPONENTS OF ZERO SHIFTS OF A THREE-AXIS LASER GYROSCOPE | 2019 |
|
RU2708689C1 |
METHOD OF CALIBRATION OF GYROSCOPES | 2001 |
|
RU2205367C1 |
INCLINOMETER | 1995 |
|
RU2111454C1 |
METHOD FOR CONTROL DESIGN OF SPACECRAFT WITH POWER GYROSCOPES AND ROTARY SOLAR PANELS | 2015 |
|
RU2614467C1 |
MAGNETOMETRIC COMPLEX FOR NAVIGATION OF OBJECTS IN SPACE | 2023 |
|
RU2808125C1 |
MOBILE ANGULAR POSITION DETECTOR RELATIVE TO GRAVITY VECTOR AND METHOD OF APPLICATION THEREOF | 2007 |
|
RU2343418C1 |
ON GROUND ASTRONOMIC AZIMUTH AND DEVIATION ANGLES OF ITS COORDINATE SYSTEM RELATIVELY GRAVITY VECTOR GRAVIMETRIC DETECTOR | 2004 |
|
RU2260176C1 |
METHOD TO DETERMINE AIRCRAFT (OR ITS MOCK-UP) ANGULAR POSITION IN SPACE | 2009 |
|
RU2395427C1 |
Authors
Dates
2017-02-28—Published
2015-12-28—Filed