Inertial Labs INS-B – Basic Single Antenna GPS-Aided Inertial Navigation System
$ 0,00
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.
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
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 |