Survey+ V3

GNSS/INS for land and airborne survey applications

Survey+ inertial navigation systems from Oxford Technical Solutions combine the best of GNSS positioning technology with high-grade gyros and accelerometers to deliver superior performance in a single enclosure. The OxTS flagship, high accuracy INS for land-based and manned aircraft mapping.

Oxford Technical Solutions - OxTS

Bicester, GB

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Description

Key Features

1 cm positioning
0.03° roll and pitch
Low cost, high accuracy
Tightly coupled GNSS/INS
gx/ix™ technology
Real-time outputs
100 or 250 Hz versions
Dual antenna versions
GLONASS enabled versions
Smooth, stable outputs
Odometer input
ITAR free
Software suite included
Cables and antennas included

OxTS Lidar Surveying Brochure

Download the OxTS LiDAR Surveying brochure and learn more about LiDAR Surveying using an OxTS INS. The brochure introduces the benefits of integrating the inertial data provided by an OxTS INS with raw LiDAR data. The brochure also details the currently supported LiDAR sensors

OxTS Boresight Calibration Brochure

Accurately measuring the angles between your navigation and survey devices can be difficult to get right. However, using a data-driven approach to calibrating these angles can dramatically reduce survey set-up time, increase survey repeatability and improve the final output. Read how this can be achieved with our Boresight Calibration brochure.

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Specifications

Other specifications: Graphical user interface

Y

Typical application

Mobile Mapping, Pavement Inspection, Rail Corridor Inspection, Aerial LiDAR

Distinguishable features

gx/ix tight-coupling technology, Free software suite including post-processing, 1 cm RTK position, high-grade low drift IMU, great urban performance, range of model variation to suit any budget

Export restrictions

Commercially Exportable, ITAR free

Environmental: Operating shock tolerance [g]

100

Max. rotation speed [deg/s]

100

Min. operating temperature [°C]

-10

Max. operating temperature [°C]

50

Software: Name

NAVsuite

Filtering

Y

Adaptable input signals

Y

Integrity monitoring of position input

Y

Integrity monitoring of log input

Y

Uncertainty indicators given in output

Y

GNSS aided uncertainty: Heading [deg]

0.05

Pitch [deg]

0.03

Roll [deg]

0.03

Heave: constant part [m]

0.1

Heave: variable part [%]

10

General: Year of initial development

2013

Height [m]

0.071

Width [m]

0.12

Length [m]

0.184

Weight [kg]

1.5

Min. Voltage (DC)

10

Max. Voltage (DC)

48

Power consumption [W]

14

Splashproof casting

Y

Water resistant casting

N

Type of accelerometer

MEMS

Type of gyro

MEMS

Type of application

Air, Land

GNSS Positioning Sensor: Number of integrated GNSS receivers and antenna ports

2

Tracked satellite signals

GPS L1, GPS L2, GLONASS L1, GLONASS L2, Option: Beidou L1, L2

SBAS differential signals

Y, Optional

RTK Network Compatibility

Y, Optional

Unaided uncertainty: Heading [deg]

0.1

Pitch [deg]

0.03

Roll [deg]

0.03

Data formats: NMEA formats

NMEA Standard ASCII

RTCM

Y

Other

NCOM, MCOM, TSS1, TSSHHRP, EM3000, EM1000

Inertial Measurement Unit: Accelerometer bias [µ-g]

2

gyro bias [deg/hr]

2

Calibration procedure

ISO17025, SuperCAL

GNSS positional accuracy: Horizontal Position Accuracy [ RMS in cm ]

180

Horizontal Position Accuracy (SBAS) [ RMS in cm ]

60

Horizontal Position Accuracy (RTK) [ RMS in cm ]

1