Geo-matching | Your Product Platform for Surveying, Positioning and Machine Guidance Join Geo-matching now!

Inertial Labs, Inc. OEM versions of Single & Dual Antenna GPS-Aided Inertial Navigation Systems (INS-B-OEM, INS-D-OEM, INS-DL-OEM

Small size, light weight, OEM version of GPS-Aided INS

INS-B-OEM, INS-D/DL-OEM are OEM version of new generation, single and 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 app

  • Inertial Labs, Inc. OEM versions of Single & Dual Antenna GPS-Aided Inertial Navigation Systems (INS-B-OEM, INS-D-OEM, INS-DL-OEM
Inertial Labs, Inc.
39959 Catoctin Ridge Street
20129 Paeonian Springs
United States
Contact supplier
Videos



Documents
Download brochure

Description

  • Commercially exportable Single & Dual Antenna GPS-Aided Inertial Navigation Systems
  • 85 x 47 x 36 mm size and 115 gram weight
  • Industrial & Tactical-grade IMU (1 – 3 deg/hr gyroscopes Bias in-run stability)
  • GPS, GLONASS, BEIDOU, SBAS, DGPS, RTK supported signals
  • 0.1 - 0.08 deg Heading, Pitch & Roll accuracy
  • Compatibility with LiDARs and optical cameras for remote sensing applications
  • Up to 200 Hz INS, up to 2000 Hz IMU, 50 Hz GNSS positions, 20 Hz GNSS measurements data rate
  • 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
  • Implemented ZUPT, GNSS tracking angle features
  • Full temperature calibration of all sensing elements 

Outage duration

Positioning mode

Position accuracy (meters, RMS)

Velocity accuracy (meters/sec, RMS)

Attitude accuracy (degree, RMS)

Horizontal

Vertical

Horizontal

Vertical

Pitch/Roll

Heading

0 sec

RTK

0.01

0.02

0.02

0.01

0.015

0.05

SP

1.2

1.0

0.03

0.02

0.1

0.08

PP

0.005

0.01

0.02

0.01

0.006

0.03

60 sec

RTK

7

2

0.3

0.1

0.05

0.08

SP

8

3

0.3

0.1

0.05

0.1

PP

0.3

0.2

0.03

0.05

0.01

0.05

Specifications

  • Type of application
    Air, Land
  • Year of initial development
    2016
  • Height [m]
    0.85
  • Width [m]
    0.47
  • Length [m]
    0.36
  • Weight [kg]
    115
  • Min. Voltage (AC)
    9
  • Max. Voltage (AC)
    36
  • Min. Voltage (DC)
    9
  • Max. Voltage (DC)
    36
  • Power consumption [W]
    3
  • Splashproof casting
    N
  • Water resistant casting
    N
  • Water resistance [m]
    0
  • Mean time between failures [hr]
    100000
  • Type of accelerometer
    MEMS
  • Type of gyro
    MEMS
  • Removable from base plate
    N
  • Moving parts
    N
  • Non-operating shock tolerance [g]
    1500
  • Operating shock tolerance [g]
    400
  • Min. operating temperature [°C]
    -40
  • Max. operating temperature [°C]
    75
  • Max. rotation speed [deg/s]
    950
  • NMEA formats
    NMEA 0183
  • RTCM
    Y
  • Other
    Binary, ASCII
  • Number of integrated GNSS receivers and antenna ports
    2
  • No. channels p receiver
    555
  • Tracked satellite signals
    GPS L1/L2, GLONASS L1/L2, BEIDOU B1/B2, GALILEO E1/E5, QZSS L1/L5,
  • SBAS differential signals
    Yes
  • RTK Network Compatibility
    Yes
  • Update rate [ Hz ]
    200
  • Cold start [ seconds ]
    50
  • Hot start [ seconds ]
    30
  • Horizontal Position Accuracy [ RMS in cm ]
    100
  • Horizontal Position Accuracy (SBAS) [ RMS in cm ]
    60
  • Horizontal Position Accuracy (RTK) [ RMS in cm ]
    1
  • Heading [deg]
    0.05
  • Pitch [deg]
    0.08
  • Roll [deg]
    0.08
  • Heave: constant part [m]
    0.05
  • Heave: variable part [%]
    5
  • Surge/sway [m]
    0.1
  • Increase in position uncertainty w.r.t. stand-alone GPS [m]
    6
  • Heading [deg]
    0.05
  • Pitch [deg]
    0.08
  • Roll [deg]
    0.08
  • Heave [m]
    0.05
  • Surge/sway [m]
    0.1
  • Decrease in position accuracy [m/hr]
    6
  • Heading [deg]
    0.05
  • Pitch [deg]
    0.08
  • Roll [deg]
    0.08
  • Heave [m]
    0.05
  • Surge/sway [m]
    0.1
  • Decrease in position accuracy [m/hr]
    6
  • Heading [deg]
    0.05
  • Pitch [deg]
    0.08
  • Roll [deg]
    0.08
  • Heave [m]
    0.05
  • Decrease in position accuracy [m/hr]
    6
  • Surge/sway [m]
    0.1
  • Accelerometer bias [µ-g]
    5
  • gyro bias [deg/hr]
    1
  • Calibration procedure
    Calibration is not required
  • Name
    GUI software
  • Filtering
    Y
  • Adaptable filter strength
    Kalman
  • Adaptable input signals
    Y
  • Integrity monitoring of position input
    Y
  • Integrity monitoring of log input
    Y
  • Max. number of position input signals
    10
  • Max. number of log input signals
    10
  • Maximum latency of log input [ms]
    3
  • Maximum latency of position input [ms]
    3
  • Uncertainty indicators given in output
    Yes
  • Uncertainty of time stamp for output [ms]
    0.02
  • Export restrictions
    No
  • Graphical user interface
    Y
  • Typical application
    Payloads of UAV//UAS, Remote sensing: mapping, low altitude photogrammetry, survey
  • Distinguishable features
    Very small size, high accuracy, related time (RTK) or post processing (PPK) applications

You have selected 2 products to compare you can add 4 more products