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VN-200 Rugged GPS/INS


 
General 
Product Name:VN-200 Rugged GPS/INS
Product Description:The VN-200 Rugged is a miniature high-performance GPS-Aided Inertial Navigation System that combines MEMS inertial sensors, a high-sensitivity GPS receiver, and advanced Kalman filtering algorithms to provide optimal estimates of position, velocity, and orientation for industrial applications.
Type of application:Air, Land, Marine
Year of initial development:2012
Height [m]:0.0095
Width [m]:0.033
Length [m]:0.036
Weight [kg]:0.016
Min. Voltage (AC):
Max. Voltage (AC):
Min. Voltage (DC):3.3
Max. Voltage (DC):17
Power consumption [W]:0.5
Splashproof casting:Y
Water resistant casting:N
Water resistance [m]:
Mean time between failures [hr]:
Type of accelerometer:3-axis MEMS
Type of gyro:3-axis MEMS
Removable from base plate:Y
Moving parts:N
Environmental 
Non-operating shock tolerance [g]:
Operating shock tolerance [g]:
Min. operating temperature [C]:-40
Max. operating temperature [C]:85
Max. rotation speed [deg/s]:2000
Data formats 
NMEA formats:RMC, GGA, GLL, GSA, GSV, HDG, HDT, THS, VTG, ZDA
RTCM:
Other :PASHR, TSS1
GNSS Positioning Sensor 
Number of integrated GNSS receivers and antenna ports:1
No. channels p receiver:50
Tracked satellite signals:GPS L1
SBAS differential signals:Y
RTK Network Compatibility:
Update rate [ Hz ]:5
Cold start [ seconds ]:36
Hot start [ seconds ]:1
GNSS positional accuracy 
Horizontal Position Accuracy [ RMS in cm ] :250
Horizontal Position Accuracy (SBAS) [ RMS in cm ]:200
Horizontal Position Accuracy (RTK) [ RMS in cm ]:
GNSS aided uncertainty 
Heading [deg]:0.3
Pitch [deg]:0.1
Roll [deg]:0.1
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]:2
Pitch [deg]:0.5
Roll [deg]:0.5
Heave [m]:
Surge/sway [m]:
Decrease in position accuracy [m/hr]:
Inertial Measurement Unit 
Accelerometer bias [µ-g]:40
gyro bias [deg/hr]:5
Calibration procedure:Calibrated at room temperature or over full thermal operating range (-40 C to +85 C) for bias, scale factor, misalignment and gyro g-sensitivity.
Software 
Name:
Filtering:Y
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:ITAR free
Graphical user interface:Y
Typical application:UAS, Camera/Antenna Stabilization, Ground Vehicles, Mapping, Smart Weapons
Distinguishable features:SWaP-C optimized, miniature rugged design, calibrated over temperature, onboard Extended Kalman Filter, automatic filter initialization & dynamic alignment, external GPS
 


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