Produtos — Coriolis Vibratory Gyroscopes (CVG)

INNALABS designs, produces and manufactures: single- and two-axis Coriolis Vibratory Gyroscopes (CVG) for stabilization applications.

Coriolis Vibratory Gyroscopes

Innalabs’ CVG sensitive element
Technology Review.
INNALABS presents new development: Coriolis Vibratory Gyroscopes (CVG) which are based on the control of two standing waves in a physical body. This body is a resonator which can be designed as an axisymmetrical shape or not, but only axisymmetrical shapes lead to top of the range performances. This breakthrough technology allowed substantially increase product life of the gyroscopes (MTBF > 500,000 hours) and their shock resistance (300g, 2 to 5ms). Along with these, INL-CVG gyroscopes achieved the highest Bias stability and the lowest noise among competitors in the market sector. Picture on the right shows INNALABS’ INL-CVG sensitive element which contains a resonator. This sensitive element is used whatever INNALABS’ products.

The resonator is operated on its second order resonant modes. Standing waves are therefore elliptical shape oscillations with four antinodes and four nodes located circumferentially along the rim, angle between two adjacent antinode – node being 45 deg. One of the elliptical resonant modes is excited to a prescribed amplitude. When the device rotates about its sensitive axis (along its inner stem), the resulting Coriolis forces acting on the resonator’s vibrating mass elements excite the second resonant mode. Angle between major axis of the two modes is 45 deg. A closed-loop drives the second resonant mode to zero and the force required to null this mode is proportional to the input rotation rate. Corresponding control loop system is called force-rebalanced mode. In order to provide forces and to sense induced motions, piezo-electric elements placed on the resonator are used. This electromechanical system is particularly effective and leads to low output noise and large dynamic range as required in case of demanding applications.

Applications. INNALABS’ INL-CVG gyroscopes will be found for example in the following very demanding applications, such as Platforms stabilization, Positioning and Stabilized Pointing, Gyro-stabilized balls, EO/FLIR stabilization, Railways tilt systems, Sonar stabilization, APS and DIRCM stabilization, Autopilot sensing and control, Midcourse guidance, Motion compensation, Inertial measurement units (IMU), Inertial Navigation Systems (INS & INS/GPS), Automated Guided Vehicles (AGV), Unmanned Underwater Vehicles (UUV), Unmanned Aerial Vehicles (UAV), Remotely Operated underwater Vehicles (ROV).

Preliminary Technical Specifications

Parameters Units Values
 Type   INL-CVG-G100
 Datasheet   Download PDF Download PDF
 Number of axis
  1 1
 Output format   Analog Digital
 Picture   Coriolis Vibratory Gyroscopes Coriolis Vibratory Gyroscopes
 Output interface   Differential +/- 10 VDC for full scale
(+/- 5 VDC, pins PO1 and PO2.
-/+ 5VDC, pins NO1 and NO2)
RS-232/422/485
 Output signal rate Hz - 2000 - 9000
 Temperature compensation (Bias, SF)   Yes Yes
 Measurement range deg/sec Up to ±250* Up to ±250*
 Bandwidth Hz Up to 150* Up to 150*
 In run Bias stability (room temperature, 1 sigma) deg/hr < 0.1 < 0.1
 Bias setting (at room temperature) deg/hr < 1 < 1
 Bias stability, full temperature range, 1σ deg/hr < 15 < 15
 Bias repeatability, turn-on turn-on, 1σ   < 10 < 10
 Angular Random Walk (steady conditions) deg/√hr 0.01 0.01
 Quiescent noise (0.1 – 100 Hz), RMS deg/sec < 0.01 < 0.01
 Noise under vibration (0.1 - 100 Hz),
 (12g  rms - 0 to 2000 Hz)
deg/hr/grms < 30 < 30
 Scale factor error, full temperature range % < 0.35 < 0.35
 Scale factor non linearity ppm < 1000 < 1000
 Start up time sec < 1 < 1
 Warm up time sec < 50 < 50
 Misalignment mrad < 10 < 10
 Input signal (MIL STD 461 and 1275) VDC 0 /+18 VDC to +36 VDC 0 /+18 VDC to +36 VDC
 Power consumption Watt <2.3
<2.3
 Operational temperature degC -40 to +85 -40 to +85
 Storage temperature degC -55 to +90 -55 to +90
 Vibrations, operational g RMS,Hz 12g, 1 – 2000 Hz, 10 min/axis 12g, 1 – 2000 Hz, 10 min/axis
 Vibrations, transport g RMS,Hz 3g, 1 – 2000 Hz, 1 h/axis 3g, 1 – 2000 Hz, 1 h/axis
 Shock g, ms 300g, 2 to 5ms 300g, 2 to 5ms
 MTBF, (MIL-HDBK 217F) hours 500,000 500,000
 Electromagnetic Environmental Effects   Not shielded Not shielded
 Lifetime years 17 17
 Weight (Sensitive Element) grams 71 71
 Weight (Damper) grams 26 26
 Weight (Electronics and Connector) grams 73 73
 Dimensions mm H25 x D29.4 (Sensitive Element) H25 x D29.4 (Sensitive Element)
 Built-in-self-test   Yes Yes
 In-Line-Test   Yes Yes

 * Contact us for customized parameters

 

INL-CVG-G100 Drawing (mm)
  Damper Drawing (mm)
INL-CVG-G100 Drawing   To ensure the INL-CVG-G100 performance according to its specifications, INNALABS recommends using the damper together with each gyroscope (SE).
 

Innalabs CVG damper

Click to enlarge the CVG Damper Drawing

Ask a question: