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Dual-antenna GPS/INS with IMU fusion · 0.2 deg (1 sigma)

Material reference: RS-INS-001-01. Brand: ROGERSENSE. Hardware and document revision are confirmed for each project.
Define the sensing task, interface and installation requirements with our engineering team.
Model-specific values and conditions. Unconfirmed values are marked TBD.
| Parameter | Published value / condition | Ref. |
|---|---|---|
| Architecture | Dual-antenna GPS/INS with IMU fusion · Manufacturer product introduction | N1 |
| Roll / pitch | 0.2 deg (1 sigma) | N1 |
| GNSS heading | 0.08 deg (1 sigma) · 2 m antenna baseline; not a free-inertial heading claim | N1 |
| GNSS position | 1.2 m CEP; RTK 2 cm + 1 ppm · Fix / correction conditions must be defined for the order | N1 |
| Gyroscope range | 300 deg/s as listed · Sign / full-scale definition TBD | N1 |
| Accelerometer range | 4 g as listed · Do not transfer specifications from another IMU | N1 |
| Input voltage / current | 12 V; 0.55 A · Confirm permissible voltage tolerance | N1 |
| Main unit | 120 x 120 x 55 mm; 708 g · Main unit only; antennas and cables are additional | N1 |
| Connector | 10-pin aviation connector · Pinout and communication electrical level TBD | N1 |
| GNSS heading condition | 0.08 deg, 1 sigma, with 2 m antenna baseline | N1 |
| Velocity accuracy | 0.03 m/s, 1 sigma | N1 |
| GNSS dropout / vehicle condition | CEP drift 0.2% over 1 km or 3 min with odometer; heading drift 0.15 deg per 1 min | N1 |
| GNSS signals | GPS L1/L2/L2C; BDS B1/B2 | N1 |
| Antenna / cable reference | 152 x 152 x 62.2 mm, 433.5 g each; cable 5 m, 30 g each | N1 |
| Signal / item | Source reference | Ref. |
|---|---|---|
| Data interface / pinout | TBD: official interface control document required | N1 |
Units: mm. Source dimensions only; unavailable details are TBD.
| Item | Published value / condition | Ref. |
|---|---|---|
| Main length x width x height | 120 x 120 x 55 mm | N1/N2 |
| Mounting grid | 108 x 108 mm | N2 |
| Mounting holes | 4 x diameter 5.30 mm; source calls for M5 screws | N2 |
| Base / main mass | 8 mm / 708 g | N1/N2 |
| Connector | 10-pin aviation connector; mating orientation / pinout TBD | N1 |
| Capability | How it is provided |
|---|---|
| Device interface | Refer to model-specific documentation |
| MQTT | Acquisition and gateway integration available; model-specific scope to agree |
| OTA | Firmware and update lifecycle services available; compatible device scope to agree |
Configuration and delivery contents are confirmed in the integration project; no online sample offer.
Confirm delivery →Specifications, dimensions, interface notes and available SDKs.
View documents →Dual-Antenna Aided Navigation System
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