OEM-HG1900

OEM-HG1900 MEMS IMU

The HG1900 Inertial Measurement Unit (IMU) offers a hybrid package of Honeywell's Micro Electromechanical Systems (MEMs) Gyros and RBA accelerometers. Economical, robust and small, the low power HG1900 provides high end tactical grade performance for commercial and military guidance and navigation applications. When integrated with NovAtel's Synchronous Position, Attitude and Navigation (SPAN) technology, this IMU is ideal for airborne and ground applications that require accurate 3D position, velocity and attitude data.

 

Features

  • MEMS Gyros
  • Small size and light weight
  • 10-30 VDC power input1
  • 100 Hz data rate
  • Long MTBF
  • SPAN INS functionality

Benefits

  • Excellent performance for price
  • Ideal for size constrained applications
  • Easy to integrate with SPAN GNSS receivers

Attributes

General Info

Width/Diameter (mm)
92.70
Height (mm)
79.10
Weight (g)
460.00
Typical Power Consumption (W)
3.00

IMU Data Rate

100 Hz

Gyro Type

MEMS

IMU Info

ITAR Control

Performance

Gyro Bias In-run Stability (±deg/hr):
Gyro Bias Offset (deg/hr):
Gyro Angular Random Walk (deg/√hr):
Gyro Scale Factor (ppm):
Gyro Range (±deg/s):

Accelerometer Bias (mg):
Accelerometer Scale Factor (ppm):
Accelerometer Range (±g):

1
5
0.09
150
1000

0.7
200
30

Combining SPAN and MEMS Technology

A proprietary NovAtel MEMS Interface Card (MIC) couples the HG1900 with SPAN receivers, offering a unique, powerful GNSS+INS system for weight and size constrained applications. Designed as a board stack configuration for ease of integration, the MIC interfaces directly with NovAtel's small form factor OEM615™ SPAN receiver.

The HG1900 is also available as a stand alone product so integrators can easily pair it with an existing OEM6® SPAN receiver.

Require Higher Accuracy?

NovAtel's CORRECT™ with RTK and satellite augmentation systems such as SBAS can be used to improve real-time performance and accuracy. For the most demanding applications, Inertial Explorer® post-processing software from our Waypoint® Products Group offers the highest level of accuracy.

Variants

OEM-HG1900
Gyro-based MEMS IMU manufactured by Honeywell. Economical, robust and small in size, the low power HG1900 provides high end tactical grade performance for commercial and military guidance and navigation applications
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General Info

Width/Diameter (mm)92.70
Height (mm)79.10
Weight (g)460.00
Typical Power Consumption (W)3.00

IMU Data Rate

100 Hz
 

Gyro Type

MEMS
 

IMU Info

ITAR Control
 

Supporting Products

Other product categories which are required with this product to create a complete system.

Vexxis Series
Antennas

GNSS receiver performance is dependent on your choice of antenna. We offer high performance, compact, low cost and ground reference station antennas. Our anti-jam antenna is available for military or homeland security applications

ProPak6.png
SPAN Receivers

SPAN capable GNSS receivers including board level and board + enclosure products

MIC.png
MEMS Interface Card

The compact, lightweight MIC supports power and communication functions of our SPAN MEMS solutions.

Alternate Products

Other similar products which could be used instead of the product, depending on application.

SPAN-CPT.png
SPAN-CPT

Single Enclosure GNSS + INS Receiver Delivers 3D Position, Velocity and Attitude

 

IMU-CPT1.png
IMU-CPT

Stand-alone OEM IMU based on NovAtel's SPAN-CPT. Comprised of fiber-optic gyros and MEMS accelerometers

HG-1930.png
OEM-HG1930

Small, Affordable MEMS IMU Pairs with SPAN Technology to Deliver 3D Position, Velocity and Attitude

LN 200 1
IMU-LN200

Tactical Grade, Low Noise IMU Combines with NovAtel's GNSS Technology to Provide 3D Position, Velocity and Attitude Solution

UIMU.png
UIMU-H58

Economical, tactical grade OEM IMUs from Honeywell

UIMU.png
UIMU-H62

Economical, tactical grade OEM IMUs from Honeywell

Optional Products

Optional products can be added to a system to add or enhance functionality.

InertialExplorerv3.png
Inertial Explorer®

Expands on the powerful features of GrafNav by adding support for loosely coupled and tightly coupled GNSS/Inertial processing