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INS-DH-OEM

The new generation of dual GNSS antenna, fully-integrated, combined GPS, GLONASS, GALILEO and BEIDOU GNSS and high-performance strapdown system, that determines position, velocity and absolute orientation (Heading, Pitch and Roll) for any device on which it is mounted.

The Inertial Labs INS-DH-OEM utilizes an advanced dual antenna GNSS receiver, a Honeywell HG4930 IMU which has 3-axes each of calibrated in full operational temperature range Advanced MEMS Accelerometers and new generation of tactical grade MEMS Gyroscopes to provide accurate Position, Velocity, Heading, Pitch and Roll of the device under measure. INS-DH-OEM contains Inertial Labs new on-board sensors fusion filter, state-of-the-art navigation and guidance algorithms and calibration software.

Description

The Inertial Labs GPS-Aided Inertial Navigation System (INS-DH-OEM) is an OEM version of the new generation of dual GNSS antenna, fully integrated, combined GPS, GLONASS, GALILEO and BEIDOU GNSS and high-performance strapdown system, that determines position, velocity and absolute orientation (Heading, Pitch and Roll) for any device on which it is mounted. Horizontal and Vertical Position, Velocity, Dual Antenna Heading, Pitch & Roll are determined with high accuracy for both motionless and dynamic applications with IMU input from the Honeywell HG4930 aided by the NovAtel Dual Antenna Receiver.

 KEY FEATURES, BENEFITS & FUNCTIONALITY

  • Commercially exportable Dual Antenna GPS-Aided Inertial Navigation System
  • Small size & lightweight: 85.5 x 67.5 x 52.0 mm size and 280-gram weight
  • Honeywell HG4930-CA51 IMU
  • Dual Antenna NovAtel GNSS Receiver for Highly Accurate Heading & Position
  • GPS, GLONASS, GALILEO, BEIDOU and QZSS constellations
  • SBAS, DGPS, RTK and PPP correction signals
  • Compatibility with most commercially available LiDARs (Velodyne, RIEGL, FARO etc.)
  • High-precision trigger for optical cameras
  • Up to 600Hz IMU; 200Hz INS and up to 100Hz GNSS data rate
  • GNSS measurements and IMU raw data for post-processing
  • Advanced, extendable, embedded Kalman Filter-based sensor fusion algorithms
  • State-of-the-art algorithms for different dynamic motions of Vessels, Ships, Helicopters, UAV, UUV, UGV, AGV, ROV, Gimbals
  • and Land Vehicles
  • Full temperature calibration of all sensing elements

Do you have questions about this product?

  • Questions about price, availability, and/or retailers
  • Questions about technical specifications and usage
  • Questions about suitability for your project or application

Specifications

Other specifications

Export restrictions

ITAR Free

Graphical user interface

Y

Typical application

Vessels, Ships, Helicopters, UAV, UUV, UGV, AGV, ROV, Gimbals and Land Vehicles

Distinguishable features

Commercially exportable High Performance Dual Antenna GPS-Aided Inertial Navigation System

Environmental

Min. operating temperature [°C]

-40

Max. operating temperature [°C]

85

Software

Name

Inertial Labs GUI

Filtering

Y

Adaptable input signals

Y

Integrity monitoring of position input

Y

Integrity monitoring of log input

Y

GNSS aided uncertainty

Heading [deg]

0.05

Pitch [deg]

0.03

Roll [deg]

0.03

General

Type of application

Air, Land, Marine

Year of initial development

2020

Height [mm]

52

Width [mm]

67.5

Length [mm]

85.5

Weight [kg]

0.28

Min. Voltage (DC)

9

Max. Voltage (DC)

34

Power consumption [W]

3.9

Splashproof casting

Y

Mean time between failures [hr]

100000

Type of accelerometer

MEMS

Type of gyro

MEMS

Moving parts

N

GNSS Positioning Sensor

Number of integrated GNSS receivers and antenna ports

2

No. channels p receiver

2

Tracked satellite signals

GPS L1 C/A, L1C, L2C, L2P, L5; GLONASS L1 C/A, L2 C/A, L2P, L3, L5; BeiDou B1, B2; Galileo E1, E5 AltBOC, E5a, E5b; NavIC (IRNSS) L5; SBAS L1, L5 QZSS L1 C/A, L1C, L2C, L5; L-Band up to 5 channels; DGPS

SBAS differential signals

L1, L5

RTK Network Compatibility

RTCM 2.1/2.3/3.0/3.1

Update rate [ Hz ]

100

Cold start [ seconds ]

39

Hot start [ seconds ]

20

Data formats

NMEA formats

Binary, TSS-1, NMEA 0183 ASCII characters

RTCM

Y

Inertial Measurement Unit

Accelerometer bias [µ-g]

25

gyro bias [deg/hr]

0.25

Calibration procedure

Full temperature calibration of all sensing elements

GNSS positional accuracy

Horizontal Position Accuracy [ RMS in cm ]

120

Horizontal Position Accuracy (SBAS) [ RMS in cm ]

60

Horizontal Position Accuracy (RTK) [ RMS in cm ]

1

Documents

Brochure
ins-dh-oem-datasheet-rev1-8-march-2021.pdf
1.61 MB
ins-dh-oem-datasheet-rev1-8-march-2021.pdf

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