| Product | Temp Compensated Accelerometer |
|---|---|
| Range | 50g |
| Scale Factor | 1.05~1.30 MA/g |
| Bias Temp Coefficient | ≤±10 μg /℃ |
| Noise | ≤5mv |
| Product Name | Dynamic Navigation Inertial Sensor |
|---|---|
| Static Accuracy | <1’ |
| Dynamic Accuracy | <2' |
| Measuring Range | ±5 ° |
| Preparation Time | <60s |
| Function | Inertial Navigation System |
|---|---|
| Range | 30g |
| Material | Stainless Housing |
| Bias | 10mg |
| Working Temp. | -40℃+150℃ |
| Sensor Name | Quartz Accelerometer |
|---|---|
| Range | 50g |
| Bias K0/K1 | ≤±5 Mg |
| Scale Factor | 0.8~1.5 MA/g |
| Weight | ≤80g |
| Product Name | Military Quartz Accelerometer |
|---|---|
| Application | Inertial Navigation |
| 0g 4hours Short-term Stability | ≤30 μg |
| Bias Thermal Coefficient | ≤±80 μg /℃ |
| Scale Factor Thermal Coefficient | ≤±100 Ppm /℃80 |
| Product Name | INS Navigation System |
|---|---|
| Positioning Accuracy | 1.5nm/h |
| Heading Accuracy | 0.1° |
| Attitude Accuracy | 0.03° |
| Speed Accuracy | 0.1m/s(RMS) |
| Product Name | Fiber Optic Inertial Navigation System |
|---|---|
| Gyro Range | ±500°/s |
| Gyro Zero Bias Stability | ±0.02°/h |
| Random Walk | ≤0.0015°/√h |
| Gyro Bandwidth | >300Hz |
| Power | ±12~±15V |
|---|---|
| Bias Thermal Coefficient | ≤±10 μg /℃ |
| Scale Factor Kl | 1.05~1.30 MA/g |
| Threshold /Resolution | 1μg |
| 0g 4 Hours Short Time Stability | ≤10 μg |
| Power Supply Voltage | 3V~3.6V |
|---|---|
| Working Temperature | -40~70℃ |
| Accelerometer Measure Range | 16g |
| Accelerometer Allan Variance | 0.015mg |
| Gyro Scale Factor Nonlinearity | 0.01%FS |
| Bias K0/k1 | ≤±2mg |
|---|---|
| Repeatability Of Scale Factor Sigma Kl/kl( 1σ，one Month) | ≤15ppm |
| 0g 4 Hours Short Time Stability | ≤10μg |
| Bandwidth | 800~2500Hz |
| Threshold /Resolution | 1μg |
