Small Size INS AFS-060
This product is mainly composed of low precision three-axis integrated fiber optic gyroscope, MEMS accelerometer and dual antenna satellite navigation module.It has all-weather autonomous navigation capability,with the ability to accept external GNSS satellite navigation parameters such as position, speed, heading, angular speed, acceleration, etc.for the carrier, and is an important information source to realize navigation positioning, guidance, control and other functions.
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Overview
Specifications
| Parameter | Value |
|---|---|
| Alignment method and Alignment time-Normal compass alignment | ≤5 min |
| Alignment method and Alignment time-Moving base transfer alignment | ≤3 min |
| Alignment method and Alignment time-Dual antenna satellite assisted alignment | ≤3 min |
| Alignment accuracy-Attitude accuracy(1σ) | ≤0.3 |
| Alignment accuracy-Azimath accuracy on single antenna satellite(1σ) | ≤1 |
| Alignment accuracy-Azimath accuracy on dual antenna satellite(1σ) | ≤0.1/R(R is the distance of dual antenna satellite) |
| Positional accuracy(CEP) [Pure inertial navigation indicators for15minutes] | ≤5 n mile |
| Velocity accuracy(RMS) [Pure inertial navigation indicators for15minutes] | ≤5 m/s |
| Attitude accuracy(RMS) [Pure inertial navigation indicators for15minutes] | ≤0.2 |
| Azimath accuracy(RMS) [Pure inertial navigation indicators for15minutes] | ≤0.4 |
| Positional accuracy(RMS) [Satellite integrated navigation indicators for1 hour] | ≤1.5 m |
| Velocity accuracy(RMS) [Satellite integrated navigation indicators for1 hour] | ≤0.03 m/s |
| Attitude accuracy(RMS) [Satellite integrated navigation indicators for1 hour] | ≤0.1 |
| Azimath accuracy(RMS) [Satellite integrated navigation indicators for1 hour] | ≤0.3 |
| Power Supply | 12~36 V |
| Power dissipation | ≤9 W |
| Work temperature | -40～+70 ℃ |
| Weight | ≤0.4 kg |
| Electrical interface | RS422,RS232 |
| Boundary Dimension | ≤63*63*70 |
| Installation Dimension | 55±0.1 mm × 55±0.1 mm |
Datasheet
Supplier Information
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