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Advanced Navigation Spatial Dual

Spatial Dual is a ruggedized miniature GPS aided inertial navigation system and AHRS that provides accurate position, velocity, acceleration and orientation under the most demanding conditions. It combines temperature calibrated accelerometers, gyros

  • Advanced Navigation Spatial Dual
Advanced Navigation
Level 8 / 37 Pitt St
2000 Sydney
Australia
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Description

Spatial Dual is a ruggedized miniature GPS aided inertial navigation system and AHRS that provides accurate position, velocity, acceleration and orientation under the most demanding conditions. It combines temperature calibrated accelerometers, gyroscopes, magnetometers and a pressure sensor with a dual antenna RTK GNSS receiver. These are coupled in a sophisticated fusion algorithm to deliver accurate and reliable navigation and orientation.

Specifications

  • Year of initial development
    2013
  • Height [m]
    0.09
  • Width [m]
    0.127
  • Length [m]
    0.031
  • Weight [kg]
    0.285
  • Min. Voltage (AC)
    0
  • Max. Voltage (AC)
    0
  • Min. Voltage (DC)
    9
  • Max. Voltage (DC)
    36
  • Power consumption [W]
    2.64
  • Splashproof casting
    Y
  • Water resistant casting
    Y
  • Water resistance [m]
    1
  • Mean time between failures [hr]
    50000
  • Type of accelerometer
    MEMS
  • Type of gyro
    MEMS
  • Removable from base plate
    N
  • Type of application
    Air, Land, Marine, Space
  • Moving parts
    N
  • Non-operating shock tolerance [g]
    2000
  • Operating shock tolerance [g]
    2000
  • Max. rotation speed [deg/s]
    2000
  • Min. operating temperature [°C]
    -40
  • Max. operating temperature [°C]
    85
  • NMEA formats
    GPZGA, GPGGA, GPVTG, GPRMC, GPHDT, PASHR
  • RTCM
    Y
  • Other
    custom formats on request
  • Heading [deg]
    0.1
  • Pitch [deg]
    0.1
  • Roll [deg]
    0.1
  • Heave: constant part [m]
    0.05
  • Heave: variable part [%]
    5
  • Surge/sway [m]
    0
  • Increase in position uncertainty w.r.t. stand-alone GPS [m]
    1.2
  • Heading [deg]
    0
  • Pitch [deg]
    0
  • Roll [deg]
    0
  • Heave [m]
    0
  • Surge/sway [m]
    0
  • Decrease in position accuracy [m/hr]
    0
  • Heading [deg]
    0
  • Pitch [deg]
    0
  • Roll [deg]
    0
  • Heave [m]
    0
  • Surge/sway [m]
    0
  • Decrease in position accuracy [m/hr]
    0
  • Heading [deg]
    0.1
  • Pitch [deg]
    0.1
  • Roll [deg]
    0.1
  • Heave [m]
    0.05
  • Surge/sway [m]
    0
  • Decrease in position accuracy [m/hr]
    0
  • Accelerometer bias [µ-g]
    20
  • gyro bias [deg/hr]
    3
  • Calibration procedure
    Not required
  • Name
    Spatial Dual Manager
  • Filtering
    Y
  • Adaptable filter strength
    Yes, user configurable profiles and settings
  • Adaptable input signals
    Y
  • Integrity monitoring of position input
    Y
  • Integrity monitoring of log input
    Y
  • Max. number of position input signals
    1
  • Max. number of log input signals
    1
  • Maximum latency of position input [ms]
    0
  • Maximum latency of log input [ms]
    0
  • Uncertainty indicators given in output
    Yes
  • Uncertainty of time stamp for output [ms]
    0.02
  • Graphical user interface
    Y
  • Typical application
    Stationary or slow moving vehiclesApplications in high magnetic interferenceApplications where FOG is too expensive or unsuitableApplications requiring vehicle slip angle measurement
  • Distinguishable features
    Dual antenna GPSDual antenna headingExtremely high accuracyNot susceptible to magnetic heading issues
  • Export restrictions
    None
  • Number of integrated GNSS receivers and antenna ports
    2
  • Tracked satellite signals
    GPS L1, GPS L2, GPS L5, GLONASS L1, GLONASS L2, Galileo E1, Galileo E5, BeiDou B1, BeiDou B2
  • SBAS differential signals
    Y
  • RTK Network Compatibility
    Y
  • Update rate [ Hz ]
    20
  • Cold start [ seconds ]
    30
  • Hot start [ seconds ]
    3
  • Horizontal Position Accuracy [ RMS in cm ]
    120
  • Horizontal Position Accuracy (SBAS) [ RMS in cm ]
    0.5
  • Horizontal Position Accuracy (RTK) [ RMS in cm ]
    0.8

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