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Inertial Labs INS-B – Basic Single Antenna GPS-Aided Inertial Navigation System

Cost effective GPS/GLONASS/BEIDOU/GALILEO-Aided Inertial Navigation System (INS-B)

The Inertial Labs Single Antenna GPS-Aided Inertial Navigation System "INS-B" is new generation of fully-integrated, combined GPS, GLONASS, GALILEO, QZSS, BEIDOU and L-Band navigation 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 and Orientation are determined with high accuracy for both motionless and dynamic applications.

  • Inertial Labs INS-B – Basic Single Antenna GPS-Aided Inertial Navigation System
Inertial Labs
39959 Catoctin Ridge Street
20129 Paeonian Springs
United States
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The Inertial Navigation System - Unboxing and Connecting
The Inertial Navigation System - Unboxing and Connecting

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Description

  • Affordable price
  • Excellent accuracy in GPS-Denied environments (Tactical-grade IMU + Aiding data)
  • GPS, GLONASS, GALILEO, BEIDOU, SBAS, DGPS, RTK supported signals
  • Tactical-grade IMU (1 deg/hr gyroscopes and 5 micro gaccelerometers Bias in-run stability)
  • High precision single antenna GNSS receivers
  • Compatibility with LiDARs (Velodyne, RIEGL, FARO) and optical cameras
  • Odometer, Wheel sensor, Airspeed sensor, Wind sensor, Doppler shift from locator aiding data
  • 1 cm + 1 ppm RTK Horizontal Position Accuracy
  • 2.5 cm TerraStar-C PRO Horizontal Position Accuracy
  • 0.1 deg GNSS Heading accuracy
  • 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 
  • Environmentally sealed (IP67), compact design, MIL-STD-810G/DO-160E

Specifications

  • Type of application
    Air, Land, Marine
  • Year of initial development
    2014
  • Height [m]
    0.053
  • Width [m]
    0.05
  • Length [m]
    0.12
  • Weight [kg]
    0.22
  • Min. Voltage (DC)
    9
  • Max. Voltage (DC)
    36
  • Power consumption [W]
    6
  • Splashproof casting
    Y
  • Water resistant casting
    Y
  • Water resistance [m]
    0.5
  • 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]
    5000
  • Operating shock tolerance [g]
    1500
  • Min. operating temperature [°C]
    -40
  • Max. operating temperature [°C]
    75
  • Max. rotation speed [deg/s]
    450
  • NMEA formats
    NMEA 0183
  • RTCM
    Y
  • Other
    Binary, ASCII
  • Number of integrated GNSS receivers and antenna ports
    1
  • No. channels p receiver
    555
  • Tracked satellite signals
    GPS, GLONASS, GALILEO, BEIDOU
  • 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]
    0.1
  • 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]
    1
  • Heading [deg]
    0.1
  • Pitch [deg]
    0.08
  • Roll [deg]
    0.08
  • Heave [m]
    0.05
  • Surge/sway [m]
    0.1
  • Decrease in position accuracy [m/hr]
    100
  • Heading [deg]
    0.1
  • Pitch [deg]
    0.08
  • Roll [deg]
    0.08
  • Heave [m]
    0.05
  • Surge/sway [m]
    0.1
  • Decrease in position accuracy [m/hr]
    100
  • Heading [deg]
    0.1
  • Pitch [deg]
    0.08
  • Roll [deg]
    0.08
  • Heave [m]
    0.05
  • Decrease in position accuracy [m/hr]
    100
  • Surge/sway [m]
    0.1
  • Accelerometer bias [µ-g]
    5
  • gyro bias [deg/hr]
    1
  • 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
    UAV, UUV, UGV, AGV, ROV
  • Distinguishable features
    Aiding data
Inertial Labs INS-D
Inertial Labs INS-D

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