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Orion INS


 
General 
Product Name:Orion INS
Product Description:RLG Inertial Navigation System: The Orion INS is meeting the needs of users in the offshore subsea construction and survey industries who need a dependable and competitively priced reference system. It can provide precise attitude, heading and heave data and is suitable for a wide range of applications such as supporting multibeam sonar surveys or the construction of major seabed installations.
Type of application:Marine
Year of initial development:2007
Height [m]:0.18
Width [m]:0.24
Length [m]:0.38
Weight [kg]:13
Min. Voltage (AC):
Max. Voltage (AC):
Min. Voltage (DC):18
Max. Voltage (DC):36
Power consumption [W]:20
Splashproof casting:Y
Water resistant casting:N
Water resistance [m]:
Mean time between failures [hr]:30000
Type of accelerometer:Honeywell Q-Flex
Type of gyro:Honeywell Digital RLG
Removable from base plate:N
Moving parts:
Environmental 
Non-operating shock tolerance [g]:
Operating shock tolerance [g]:
Min. operating temperature [C]:-15
Max. operating temperature [C]:55
Max. rotation speed [deg/s]:200
Data formats 
NMEA formats:
RTCM:
Other :
GNSS Positioning Sensor 
Number of integrated GNSS receivers and antenna ports:
No. channels p receiver:
Tracked satellite signals:
SBAS differential signals:
RTK Network Compatibility:
Update rate [ Hz ]:
Cold start [ seconds ]:
Hot start [ seconds ]:
GNSS positional accuracy 
Horizontal Position Accuracy [ RMS in cm ] :
Horizontal Position Accuracy (SBAS) [ RMS in cm ]:
Horizontal Position Accuracy (RTK) [ RMS in cm ]:
GNSS aided uncertainty 
Heading [deg]:
Pitch [deg]:
Roll [deg]:
Heave: constant part [m]:
Heave: variable part [%]:
Surge/sway [m]:
Increase in position uncertainty w.r.t. stand-alone GPS [m]:
EM log aided uncertainty 
Heading [deg]:
Pitch [deg]:
Roll [deg]:
Heave [m]:
Surge/sway [m]:
Decrease in position accuracy [m/hr]:
Doppler log aided uncertainty 
Heading [deg]:
Pitch [deg]:
Roll [deg]:
Heave [m]:
Surge/sway [m]:
Decrease in position accuracy [m/hr]:
Unaided uncertainty 
Heading [deg]:0.1
Pitch [deg]:0.01
Roll [deg]:0.01
Heave [m]:0.05
Surge/sway [m]:0.05
Decrease in position accuracy [m/hr]:
Inertial Measurement Unit 
Accelerometer bias [µ-g]:
gyro bias [deg/hr]:
Calibration procedure:
Software 
Name:OrionView
Filtering:
Adaptable filter strength:
Adaptable input signals:
Integrity monitoring of position input:
Integrity monitoring of log input:
Max. number of position input signals:
Max. number of log input signals:
Maximum latency of position input [ms]:
Maximum latency of log input [ms]:
Uncertainty indicators given in output:
Uncertainty of time stamp for output [ms]:
Other specifications 
Export restrictions:
Graphical user interface:Y
Typical application:
Distinguishable features:
 


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