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Inertial Labs IMU-NAV-100

Navigation Grade MEMS Inertial Measurement Units: Tactical A – for Guidance & Navigation, Tactical S – for Stabilization and Pointing

The Inertial Labs IMU-NAV is a breakthrough, fully integrated inertial solution that combines the latest MEMS sensor technologies. Fully calibrated, temperature compensated, mathematically aligned to an orthogonal coordinate system, the IMU contains up to 0.5 deg/hr gyroscopes and 0.003 mg bias in-run stability accelerometers with very low noise and high reliability.

  • Inertial Labs IMU-NAV-100
Inertial Labs
39959 Catoctin Ridge Street
20129 Paeonian Springs
United States
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Description

The Inertial Labs Inertial Measurement Unit (IMU-NAV) is the latest addition to the Inertial Labs Advanced MEMS sensor-based family. Revolutionary due to its compact, self-contained strapdown, tactical grade Inertial Measurement Systems and Pitch & Roll Sensor, that measures linear accelerations, angular rates, Pitch & Roll with three-axis high-grade MEMS accelerometers and three-axis tactical grade MEMS gyroscopes. Angular rates and accelerations are determined with high accuracy for both motionless and dynamic applications.

Continuous Built-in Test (BIT), configurable communications protocols, electromagnetic interference (EMI) protection, and flexible input power requirements make the Inertial Labs IMU-NAV easy to use in a wide range of higher order integrated system applications.

The Inertial Labs IMU-NAV models were designed for applications, like:

  • Antenna and Line of Sight Stabilization Systems
  • Passenger trains acceleration / deceleration and jerking systems
  • Motion Reference Units (MRU)
  • Motion Control Sensors (MCS)
  • Gimbals, EOC/IR, platforms orientation and stabilization
  • GPS-Aided Inertial Navigation Systems (INS)
  • Attitude and Heading Reference Systems (AHRS)
  • Land vehicles navigation and motion analysis
  • Buoy or Racing Boat Motion Monitoring
  • UAV & AUV/ROV navigation and control

Specifications

  • Year of last update
    2021
  • Year of initial development
    2020
  • System components
    Accelerometer(s), Gyroscope(s), Temperature sensor
  • Height [mm]
    59.2
  • Width [mm]
    48.2
  • Length [mm]
    48.2
  • Weight [gr]
    155
  • Min. Voltage (DC)
    5
  • Max. Voltage (DC)
    30
  • Power consumption [W]
    0.8
  • Min. operating temperature [C]
    -40
  • Max. operating temperature [C]
    85
  • Splashproof casting
    Y
  • Water resistant casting
    N
  • Casting and coating
    IP67
  • Vibration
    7g, 20 – 2000 Hz
  • Shock
    1500g
  • Interface types
    Digital
  • Interfaces
    RS-322, RS-422
  • Output data formats
    Accelerations, Angular rates, Pitch, Roll, Relative Heading, Temperature, Synchronization output
  • Output frequency [ Hz ]
    2000
  • Max. rotation speed [deg/s]
    950
  • Start up time [s]
    1
  • Pitch and Roll dynamic accuracy [ ° ]
    0.06
  • Pitch and Roll static accuracy [ ° ]
    0.03
  • Num. of Gyroscopes
    3
  • Range [± ° / sec]
    950
  • In-Run Bias Stability [ °/ hr]
    0.5
  • Bandwidth [ Hz ]
    260
  • Non-linearity [ % ]
    0.01
  • Alignment Error [ ± ° ]
    0.0086
  • Resolution [ ° / s ]
    0.01
  • Noise
    0.1 deg/√hr for Tactical A, 0.04 deg/√hr for Tactical S
  • Distinguishable features
    ITAR free, Navigation Grade, MIL-STD-810G compliant
  • Application
    Antenna and Line of Sight Stabilization Systems ❖ Passengers trains acceleration / deceleration and jerking systems ❖ Motion Reference Units (MRU) ❖ Motion Control Sensors (MCS) ❖ Gimbals, EOC/IR, platforms orientation and stabilization ❖ GPS-Aided Inertial Navigation Systems (INS) ❖ Attitude and Heading Reference Systems (AHRS) ❖ Land vehicles navigation and motion analysis ❖ Buoy or Racing Boat Motion Monitoring ❖ UAV & AUV/ROV navigation and control
  • Num. of Accelerometers
    3
  • Range [max g]
    40
  • Bandwidth [ Hz ]
    260
  • Alignment Error [ ± ° ]
    0.0086
  • In-Run Bias Stability [mg]
    0.015
  • Non-linearity [ % ]
    0.015
  • Noise
    0.025 m/sec/√hr
Inertial Labs INS-D
Inertial Labs INS-D

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