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RS-INS-001-01 Dual-Antenna Aided Navigation System

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

RS-INS-001-01 Dual-Antenna Aided Navigation System

Material reference: RS-INS-001-01. Brand: ROGERSENSE. Hardware and document revision are confirmed for each project.

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Define the sensing task, interface and installation requirements with our engineering team.

ROGERSENSE specifications

Model-specific values and conditions. Unconfirmed values are marked TBD.

ParameterPublished value / conditionRef.
ArchitectureDual-antenna GPS/INS with IMU fusion · Manufacturer product introductionN1
Roll / pitch0.2 deg (1 sigma)N1
GNSS heading0.08 deg (1 sigma) · 2 m antenna baseline; not a free-inertial heading claimN1
GNSS position1.2 m CEP; RTK 2 cm + 1 ppm · Fix / correction conditions must be defined for the orderN1
Gyroscope range300 deg/s as listed · Sign / full-scale definition TBDN1
Accelerometer range4 g as listed · Do not transfer specifications from another IMUN1
Input voltage / current12 V; 0.55 A · Confirm permissible voltage toleranceN1
Main unit120 x 120 x 55 mm; 708 g · Main unit only; antennas and cables are additionalN1
Connector10-pin aviation connector · Pinout and communication electrical level TBDN1
GNSS heading condition0.08 deg, 1 sigma, with 2 m antenna baselineN1
Velocity accuracy0.03 m/s, 1 sigmaN1
GNSS dropout / vehicle conditionCEP drift 0.2% over 1 km or 3 min with odometer; heading drift 0.15 deg per 1 minN1
GNSS signalsGPS L1/L2/L2C; BDS B1/B2N1
Antenna / cable reference152 x 152 x 62.2 mm, 433.5 g each; cable 5 m, 30 g eachN1

Interface & connection reference

Signal / itemSource referenceRef.
Data interface / pinoutTBD: official interface control document requiredN1

Mechanical dimensions & installation

Units: mm. Source dimensions only; unavailable details are TBD.

ROGERSENSE dimension reference
ItemPublished value / conditionRef.
Main length x width x height120 x 120 x 55 mmN1/N2
Mounting grid108 x 108 mmN2
Mounting holes4 x diameter 5.30 mm; source calls for M5 screwsN2
Base / main mass8 mm / 708 gN1/N2
Connector10-pin aviation connector; mating orientation / pinout TBDN1

Documentation

Download specification · v1.0 →

Connectivity & lifecycle

CapabilityHow it is provided
Device interfaceRefer to model-specific documentation
MQTTAcquisition and gateway integration available; model-specific scope to agree
OTAFirmware and update lifecycle services available; compatible device scope to agree

Included items & evaluation steps

Dual-Antenna Aided Navigation System

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★★★★★