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LandMark™50 INS/GPS

 

Quick-Access Documents

LandMark™50 INS/GPS DataSheet PDF

LandMark™50 INS/GPS User Guide PDF

Applications

 

The LandMark™50 INS/GPS offers wide

application usage:

 

platform stabilization

EO/IR stabilization

• antenna stabilization & pointing

• railway motion monitoring

• flight control & navigation

• automotive testing

• laboratory use

 

 

Similar Products

 

LandMark™50 IMU (Inertial Measurement Unit)

LandMark™50 VG (Vertical Gyro)

LandMark™50 AHRS (Attitude & Heading

Reference System)

LandMark™50 VG/GPS (GPS-Aided

Vertical Gyro)

LandMark™50 GPS/AHRS (GPS-Aided

Attitude & Heading Reference System)

The LandMark™50 INS/GPS is Form, Fit, Function Interchangeable with the:

LandMark™30 INS/GPS

 

 

  • General
  • Features
  • Specification
  • Documentation

 

LMRK50INSGPS

LandMark™ GPS-Aided Inertial Navigation System

 

The LandMark™50 INS/GPS is the lowest noise version of our standard LandMark™ INS/GPS and now also features CANBUS output. GPS aiding is included in all units for turning error correction as well as for continued output during short-term GPS dropouts.

 

The unit features a 72 Channel GNSS: GPS, GLONASS, BeiDou, QZSS & SBAS (Galileo Ready*) with up to 18Hz GPS position update rate integrated with a high performance inertial suite that includes ultra low noise gyros and accelerometers with exceptional bias in-run and bias over temperature performance.

 

The GPS-Aided INS is highly durable and can withstand environmental vibration, shock and EMI typically associated with commercial aircraft requirements. The LandMark™ 50 INS/GPS is well suited for flight control, navigation, image & antenna stabilization and pointing, general aviation, automotive testing, as well as laboratory use.

 

 

 

 

LMRK50INSGPS

9 Degrees of Freedom MEMS INS/GPS

 

The INS/GPS performance is optimized with fully temperature compensated bias and scale factor, and compensated misalignment and g-sensitivity.

 

The unit is environmentally sealed in a rugged enclosure and Mil-Spec connector in order to withstand environmental vibration and shock typically associated with commercial aircraft requirements.


•   NON-ITAR Commercial MEMS INS/GPS

•   1°/hr in-run bias stability
•   0.0009°/sec/√Hz angle random walk

•   RS422/ RS485/CAN 2.0B Serial Data Format

•   72 Channel GNSS and up to 18Hz GPS Position Update Rate

•  GPS, GLONASS, BeiDou, and QZSS & SBAS (Galileo Ready*)

•   Simple integration supported by SDK

 

 

Available Configurations:

LMRK50INSGPS-100-02-200 or -06 or -10
LMRK50INSGPS-175-02-200 or -06 or -10
LMRK50INSGPS-300-02-200 or -06 or -10
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High Performance NON-ITAR Commercial MEMS GPS-Aided INS with CAN BUS

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5 NMPH Free Inertial (Short-Term GPS Outages)
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72 Channel GNSS: GPS, GLONASS, BeiDou, QZSS & SBAS (Galileo Ready*)
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SBAS: WAAS, EGNOS and MSAS User Selectable Option
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Up to 18 Hz GPS Position Update Rate
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GPS Velocity Accuracy 0.05 m/s
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GPS Heading Accuracy 0.3 degrees
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GPS Accuracy ± 2.5m CEP Stationary
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Ultra Low Noise Gyros 0.0009°/sec/√Hz 1σ
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Low Noise Accels 0.02mg/√Hz 1σ
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In-Run Gyro Bias 1°/hour 1σ
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Fully Compensated Bias, Scale Factor, Misalignment, g-Sensitivity, Heading & Altitude
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RS422/RS455 Serial Data Format 100Hz
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Low Power < 1 W typical
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Input Voltage +6V to +36V
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Light Weight < 450 grams
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Small Size < 360cm3/21.8in3
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Export Classification: Commerce ECCN7A994

 

 

How to Buy

 

To discuss configuration for your specific system requirements, please use our Contact page.

 

For large quantity orders or OEM discussions, please contact sales@gladiatortechnologies.com.

 

If you are outside the US, please contact one of our representatives.