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

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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.

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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


Inertial Labs GPS-Aided INS for Remote Sensing

The Inertial Navigation System (INS) – Unboxing and Connecting


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Additional information

Type of application

Air, Land, Marine

Adaptable filter strength

Kalman

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

Heave [m]

0.05

Decrease in position accuracy [m/hr]

100

Accelerometer bias [µ-g]

5

gyro bias [deg/hr]

1

Name

GUI Software

Filtering

Y

Adaptable input signals

Y

Horizontal Position Accuracy (SBAS) [ RMS in cm ]

60

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

Brand

Inertial Labs

Addres

Inertial Labs

39959 Catoctin Ridge Street

20129 Paeonian Springs

United States

Horizontal Position Accuracy (RTK) [ RMS in cm ]

1

Horizontal Position Accuracy [ RMS in cm ]

100

Year of initial development

2014

Moving parts

N

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

Non-operating shock tolerance [g]

5000

Hot start [ seconds ]

30

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

URL

https://inertiallabs.com/