GPS-Aided INS-D, INS-DL Dual Antenna

Description

The Inertial Labs Single and Dual Antenna GPS-Aided Inertial Navigation System — INS is new generation of fully-integrated, combined L1 & L2 GPS, GLONASS, GALILEO and BEIDOU navigation and high performance strapdown system, that determines position, velocity, heave and absolute orientation (Heading, Pitch and Roll) for any device on which it is mounted.

Horizontal and Vertical Position, Velocity, Heave and Orientation are determined with high accuracy for both motionless and dynamic applications.

• The GPS-Aided INS-D is a dual antenna, high precision Heading Tactical-grade IMU SP/SBAS/DGPS/RTK.
• The GPS-Aided INS-DL is a low-cost, dual antenna, high precision Heading Industrial-grade IMU with 1 cm RTK position

The Intertial Labs INS utilizes an advanced GNSS receiver, barometer, 3-axes each of calibrated in full operational temperature range precision Fluxgate magnetometers, Accelerometers, and Gyroscopes to provide accurate Position, Velocity, Heading, Pitch and Roll of the device under measure.

INS contains Inertial Labs new on-board sensors fusion filter, state of the art navigation and guidance algorithms and calibration software.

 

Click Here for GPS-Aided INS Data Sheet

 

Key Features and Functionality

• State-of-the-art algorithms for different dynamic motions of Vessels, Ships, Helicopters, UAV, UUV, UGV, AGV, ROV, Gimbals and Land Vehicles
• Single and Dual antenna GNSS receivers
• 1.5 meters L1 GPS & GLONASS Horizontal Position Accuracy
• 1.2 meters L1, L2 & GLONASS Horizontal Position Accuracy
• 60 cm SBAS Horizontal Position Accuracy
• 40 cm DGPS Horizontal Position Accuracy
• 5 cm Post Processing (PP) Horizontal Position Accuracy
• 1 cm + 1ppm RTK Horizontal Position Accuracy
• Up to 50 Hz GNSS positions data rate
• Up to 20 Hz GNSS measurements (raw) data rate
• 1 deg/hr gyroscopes Bias in-run stability
• 5 μg accelerometers Bias in-run stability
• 5% or 0.05 meters RMS (whichever is greater) Heave measurement accuracy
• 0.08 deg GNSS Heading and 0.4 deg Gyro-Stabilized Slaved Magnetic Heading accuracy (3 sigma)
• Highly accurate, reliable and temperature stable Fluxgate magnetometers (in-house technology)
• Advanced, extendable, embedded Kalman Filter based sensor fusion algorithms
• Full temperature calibration of all sensing elements
• Environmentally sealed (IP67)
• Compact design

 

 

Specifications

GNSS constellations & corrections: GPS L1/L2; GLONASS L1/L2; BeiDou B1/B2/B3; GALIILEO E1/E5; SBAS; DGPS; RTK

Position Accuracy: 1.5 m (GPS L1); 1.2 m (GPS L1/L2); 0.6 m (SBAS); 0.4 m (DGPS); 0.01 m (RTK); 0.005 m (PPK)

GNSS and IMU raw data output: YES

LiDAR & Optical camera compatibility: YES

Heading Accuracy: 0.05 deg (SP); 0.03 deg (PPK)

Pitch & Roll accuracy: 0.1 deg (SP); 0.006 deg (PPK)

IMU: Tactical-grade 1 deg/hr Gyroscopes, 0.005 mg accelerometers Bias in-run stability

Size: 120 x 50 x 53 mm

Weight: 320 gram

 

About Inertial Labs

Inertial Labs is a designer, developer and manufacturer of position and orientation tracking systems based on the combination of inertial sensors with a variety of other sensing technologies. With specific engineering expertise that includes the development of gyroscope technologies, gyro-compass systems, Kalman filter design, and sensor fusion; Inertial Labs engineers combine practical experience with PhD level academic knowledge.

KEY SPECIFICATION
Horizontal position accuracy (GPS | L1)	1.5m
Horizontal position accuracy (GPS | GLONASS | L1 | L2)	1.2m
Horizontal position accuracy (SBAS)	0.6m
Horizontal position accuracy (DGPS)	0.4m
Horizontal position accuracy (RTK)	0.01m
Position data rate	50Hz
Heave accuracy	5%
GNSS Heading accuracy	0.1°
Gyro-Stabilized Slaved Magnetic Heading accuracy	0.4°
Attitude accuracy	0.1°
Gyroscopes Bias in-run stability	4°/hr
Accelerometers Bias in-run stability	0.05mg
Input power	9 to 40 V DC
Interfaces	RS-232 | 422 | CAN 2.0
Output data format	Binary | TSS-1 | NMEA 0183