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Navigation Systems

ALR-INS SERIES

INTEGRATED NAVIGATION SYSTEMS

Scalable position, velocity, attitude and heading solutions for unmanned, airborne, land and maritime platforms.

The ALR-INS Series integrates ALR-IMU Series inertial measurement units with multi-frequency, multi-constellation RTK GNSS receivers to deliver accurate and continuous position, velocity, attitude and heading information. Comprising the ALR-INS-021, ALR-INS-031 and ALR-INS-032, the family combines different ALR-IMU performance levels with a scalable system architecture to meet the navigation requirements of land, airborne and maritime platforms. Its embedded sensor-fusion capabilities support AHRS operation, barometric aiding, dual-antenna GNSS heading, odometer, speed-log and air-data aiding, as well as transfer alignment for dynamic and mission-critical applications.

TECHNICAL PARAMETER ALR-INS-021 ALR-INS-031 ALR-INS-032
SYSTEM CONFIGURATION
Integrated IMU ALR-IMU-011 ALR-IMU-011 ALR-IMU-012
GNSS Antenna Configuration Single antenna Dual antenna Dual antenna
POSITION & VELOCITY PERFORMANCE
GNSS Position Accuracy — Horizontal / Vertical 1 m / 1.5 m 1 m / 1.5 m 1 m / 1.5 m
RTK Position Accuracy — Horizontal / Vertical 0.01 m / 0.02 m 0.01 m / 0.02 m 0.01 m / 0.02 m
Velocity Accuracy 0.05 m/s 0.05 m/s 0.05 m/s
ATTITUDE & HEADING PERFORMANCE
Pitch / Roll Accuracy 0.015° 0.1° 0.015°
Static / Dynamic Heading Accuracy — / 0.05° 1.0° / 0.15° 1.0° / 0.05°
Dual-Antenna GNSS Heading Accuracy¹ 0.15° 0.15°
NAVIGATION & AIDING FUNCTIONS
AHRS Capability
Integrated Pressure Sensor
Odometer Input
Speed-Log Input
Air-Data Input
Transfer Alignment
ELECTRICAL & COMMUNICATION INTERFACES
Supply Voltage 5 VDC 5 VDC 5 VDC
Current Consumption 175 mA 175 mA 205 mA
Communication Interfaces RS-422 / RS-485 RS-422 / RS-485 / UART RS-422 / RS-485 / UART
MECHANICAL CHARACTERISTICS
Dimensions 60 × 68 × 22 mm 42.2 × 45 × 26.7 mm 78.7 × 70.1 × 26.1 mm
Weight <150 g <200 g <200 g

¹ Specified with a 1 m antenna baseline.

Accuracy values represent typical performance under nominal operating and GNSS conditions. RTK performance requires valid correction data and suitable satellite visibility.

Product specifications are configuration-dependent and subject to change without notice.