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Inertial Labs INS-P – Professional Single Antenna GPS-Aided Inertial Navigation System

The best compact and cost effective GPS-Aided Inertial Navigation System (INS-P) for GPS-enable and GPS-denied environments

The Inertial Labs, Professional version of Single Antenna GPS-Aided Inertial Navigation System "INS-P" is the new generation of fully-integrated, combined Tactical-grade IMU, Fluxgate compass and high precision GNSS receiver, supporting GPS, Glonass, Galileo, QZSS, Beidou and L-Band navigation. INS-P is high-performance strapdown system, that determines position, velocity and absolute orientation (Heading, Pitch and Roll) for any device on which it is mounted.

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

Inertial Labs - INS for Multi Copter UAV
Inertial Labs - INS for Multi Copter UAV

Inertial Labs - INS for UAV Flight Control in GPS Denied Environments
Inertial Labs - INS for UAV Flight Control in GPS Denied Environments

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Description

  • MIL-STD-810G/DO-160E compliance
  • 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 accelerometers Bias in-run stability)
  • High precision single antenna GNSS receivers
  • The best on a market solution for UAV/UAS flight control in GPS-denied environments
  • Embedded gyro-compensated Fluxgate compass
  • 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]
    0.28
  • Min. Voltage (AC)
    9
  • Max. Voltage (AC)
    36
  • Min. Voltage (DC)
    9
  • Max. Voltage (DC)
    36
  • Power consumption [W]
    1.4
  • 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]
    3000
  • Operating shock tolerance [g]
    1500
  • 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
    1
  • No. channels p receiver
    555
  • Tracked satellite signals
    GPS L1/L2/L5; GLONASS L1/L2; BeiDou B1/B2/B3, QZSS L1/L2/L5; GALILEO E1/E5
  • 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
  • Calibration procedure
    Embedded magnetic calibration of the gyro-compensated Fluxgate compass
  • 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/UAS flight control systems
  • Distinguishable features
    Aiding data; Tactical-grade IMU; High precision GNSS receiver; gyro-compensated Fluxgate Compass
Inertial Labs INS-D
Inertial Labs INS-D

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