Produtos — Coriolis Vibratory Gyroscopes (CVG)
INNALABS designs, produces and manufactures: single- and two-axis Coriolis Vibratory Gyroscopes (CVG) for stabilization applications. |
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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-GU200 | ||
| Datasheet | Download PDF |
Download PDF |
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| Number of axis |
Two (along X and Y) | ||
| Output format | Analog | Digital |
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| Picture | ![]() |
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| 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 | > 150 | > 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 | % | < 0.1 |
< 0.1 |
| 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 | < 3.3 | < 3.3 |
| 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 | MIL-STD-461E | MIL-STD-461E | |
| Lifetime | years | 17 | 17 |
| Weight | kg | 1.1 | 1.1 |
| Dimensions | mm | H68 x L107 x W107 | H68 x L107 x W107 |
| Built-in-self-test | Yes | Yes | |
| INL-CVG-GU200 Drawing (mm) |
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