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Inertial Labs INS-DM

IP68 Super Ruggedized Dual Antenna GPS-Aided Inertial Navigation System

The Inertial Labs GPS-Aided Inertial Navigation System (INS-DM) is the latest version of Inertial Navigation System, developed by Inertial Labs. The INS-DM is the result of over 20 years of our experience in developing and supplying INS solutions to land, marine and aerial platforms around the world. The Inertial Labs GPS-Aided Inertial Navigation System (INS-DM) is the latest version of Inertial Navigation System, developed by Inertial Labs.

  • Inertial Labs INS-DM
Inertial Labs
39959 Catoctin Ridge Street
20129 Paeonian Springs
United States
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Description

This system, the INS-DM, is an IP68 rated version of an all-new generation of super ruggedized, shielded from the EMC/EMI, fully-integrated, combined Inertial Navigation System (INS) + Attitude & Heading Reference System (AHRS) + Air Data Computer (ADC) 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. 

The Inertial Labs INS-DM can support multiple types of MEMS Inertial Measurement Units (IMU) developed by Inertial Labs. Additionally, the INS-DM supports other IMU’s, like the Honeywell HG4930. The INS-DM also utilizes different multi constellation (GPS, GLONASS, GALILEO, QZSS and BEIDOU) GNSS receivers like Novatel OEM7 series or the u-blox F9 series.

The design of the INS-DM also includes an optional Air Data Computer (ADC), supported by two Honeywell barometric sensors, and the ability to support an internal Fluxgate or external Stand-Alone Magnetic Compass (SAMC). The INS-DM contains Inertial Labs new on-board sensor fusion filter, state of the art navigation and guidance algorithms, and calibration software.

KEY FEATURES, BENEFITS & FUNCTIONALITY

  • Commercially exportable GPS-Aided Inertial Navigation System
  • 3-in-1 Strapdown System: INS + AHRS + ADC (Air Data Computer)
  • Embedded industrial, tactical, or navigation grade Honeywell or Inertial Labs MEMS Inertial Measurement Unit (IMU)
  • Novatel OEM7 or u-blox ZED-F9P F9 high precision GNSS receiver
  • GPS, GLONASS, GALILEO, BEIDOU, QZSS, RTK supported signals
  • Total and static pressure sensors for calculating indicated airspeed
  • SP, SBAS, DGPS, RTK and PPP corrections supported for precise real time operation
  • GNSS measurements and IMU raw data for post processing
  • Advanced, extendable (based on application), embedded Kalman Filter based sensor fusion algorithms
  • State-of-the-art algorithms for different dynamic motions of helicopters, UAV’s, marine vessels, and ground vehicles
  • Full temperature calibration of all sensing elements
  • EMC, EMI and ERD protection (MIL-STD-1275)
  • Environmentally sealed (IP68)
  • Aiding data: Wind sensor, Air Speed Sensor, Doppler shift from locator (for long-term GPS denied), External position and External Heading

Specifications

  • Type of application
    Air, Land, Marine, Space
  • Year of initial development
    2021
  • Height [mm]
    61.1
  • Width [mm]
    141.2
  • Length [mm]
    160.4
  • Weight [kg]
    1.345
  • Min. Voltage (DC)
    9
  • Max. Voltage (DC)
    36
  • Splashproof casting
    Y
  • Water resistant casting
    Y
  • Water resistance [m]
    1.5
  • Mean time between failures [hr]
    100000
  • Type of accelerometer
    MEMS
  • Type of gyro
    MEMS
  • Removable from base plate
    N
  • Moving parts
    N
  • Min. operating temperature [°C]
    -40
  • Max. operating temperature [°C]
    80
  • NMEA formats
    NMEA 0183
  • RTCM
    Y
  • Other
    Binary
  • Number of integrated GNSS receivers and antenna ports
    2
  • No. channels p receiver
    555
  • Tracked satellite signals
    GPS L1 C/A, L1C, L2C, L2P, L5; GLONASS L1 C/A, L2 C/A, L2P, L3, L5; BeiDou B1I, B1C, B2I, B2a, B3I; Galileo E1, E5 AltBOC, E5a, E5b, E6; NavIC (IRNSS) L5; QZSS L1 C/A, L1C, L2C, L5, L6; L-Band
  • SBAS differential signals
    WAAS; EGNOS; MSAS; GAGAN; SBAS L1, L5; DGPS; RTK; PPP Terrastar
  • RTK Network Compatibility
    RTCM 2, RTCM 3
  • Update rate [ Hz ]
    100
  • Cold start [ seconds ]
    39
  • Hot start [ seconds ]
    20
  • Horizontal Position Accuracy [ RMS in cm ]
    1200
  • Horizontal Position Accuracy (SBAS) [ RMS in cm ]
    60
  • Horizontal Position Accuracy (RTK) [ RMS in cm ]
    1
  • Heading [deg]
    0.08
  • Pitch [deg]
    0.01
  • Roll [deg]
    0.01
  • Accelerometer bias [µ-g]
    0.25
  • gyro bias [deg/hr]
    0.025
  • Name
    Advanced, extendable, embedded Kalman Filter, sensor fusion algorithms
  • Filtering
    Y
  • Adaptable input signals
    Y
  • Integrity monitoring of position input
    Y
  • Export restrictions
    ITAR free
  • Graphical user interface
    Y
  • Typical application
    Land, marine and aerial platforms
  • Distinguishable features
    Aiding data: Wind sensor, Air Speed Sensor, Doppler shift from locator (for long-term GPS denied), External position and External Heading

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