SkyTraq PX1175RDP Manual

SkyTraq PX1175RDP Manual

L1/l5 gnss rtk dead reckoning receiver

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Features
Centimeter accuracy RTK dead-reckoning receiver
3-axis accelerometer & gyroscope
Barometric pressure sensor altitude sensing
Automatic sensor calibration
230 Channel receiver
GPS/Galileo/Beidou/QZSS/NavIC receiver
17mm x 22mm size
NMEA-0183 and RTCM 3.x protocol
Easy to integrate
Operating temperature -40 ~ +85ºC
RoHS compliant
Applications
4 Wheel Vehicle RTK Navigation
PX1175RDP
L1/L5 GNSS RTK
Dead Reckoning Receiver
The PX1175RDP GNSS RTK Dead-Reckoning receiver
module combines RTK position data, gyroscope data
(measuring
(measuring distance traveled) to formulate position
solution. This enables accurate navigation solution in
poor signal environment or signal blocked area. The
PX1175RDP is ideal for 4-wheel vehicle applications
requiring accurate continuous navigation.
PX1175RDP can operate in Automotive Dead Reckoning
(ADR) mode if the vehicle wheel-tick odometer signal is
connected; or operate in Odometer-less Dead Reckoning
(ODR) mode if the odometer signal is not connected.
The barometric pressure sensor provides superior
altitude sensing performance.
The Extended Kalman Filter algorithm combines GNSS
and sensor data with weighting function dependent on
GNSS signal quality. In poor signal reception area, the
position error is reduced by dead reckoning.
The PX1175RDP with dead-reckoning feature, position is
output as soon as power is applied to the module
without the need of getting GPS/GNSS position fix.
The receiver is suitable for RTK applications that require
high performance continuous positioning and velocity
data.
1
turning
angle),
and
odometer
data

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Summary of Contents for SkyTraq PX1175RDP

  • Page 1 Barometric pressure sensor altitude sensing solution. This enables accurate navigation solution in ⚫ poor signal environment or signal blocked area. The Automatic sensor calibration PX1175RDP is ideal for 4-wheel vehicle applications ⚫ 230 Channel receiver requiring accurate continuous navigation. ⚫...
  • Page 2: Technical Specifications

    Protocol NMEA-0183 V4.1 GGA, GLL, GSA, GSV, RMC, VTG 115200 baud, 8, N, 1 RTCM 3.x or SkyTraq raw data binary 115200 baud, 8, N, 1 Datum Default WGS-84 and user definable in stand-alone mode Depends on base reference frame when in RTK mode Input Voltage 3.3V +/- 10%...
  • Page 3: Block Diagram

    BLOCK DIAGRAM Module block schematic Active antenna is required to use with PX1175RDP. The received signal goes through a signal splitter, to individual L1 and L2/L5 SAW filters to remove out-band interference, then to the PX100-5R-01A GNSS receiver chip for RTK signal processing. Using correction data from an RTK base station, the PX1175RDP computes the antenna position to centimeter-level accuracy relative to the base station.
  • Page 4 SUPPORTED RTCM MESSAGES When operating in rover mode, PX1175RDP can decode following RTCM 3.3 messages: RTCM Message Type Description 1005 Stationary RTK reference station antenna reference point 1006 Stationary RTK reference station ARP with antenna height 1033 Receiver and antenna description...
  • Page 5: Pinout Description

    PINOUT PINOUT DESCRIPTION Pin No. Name Description Ground RF input RF_IN RTK Position: RF_IN antenna position Ground No connection, empty pin 4,5,6 Voltage for external LNA VCC_RF No connection, empty pin 8,9,10,11 Ground No connection, empty pin Ground No connection, empty pin UART serial data input, 3.3V LVTTL.
  • Page 6 HIGH. If the driving circuitry is powered independently of PX1175RDP, ensure that this pin is not driven to HIGH when PX1175RDP is put to sleep, or a 10K-ohm series resistor can be added to minimize leakage current.
  • Page 7 No connection, empty pin 46,47 Ground External active-low reset input to the baseband. RSTN Only needed when power supply rise time is very slow or software controlled reset is desired. No connection for normal use. Pull-low for loading firmware into empty or BOOT_SEL corrupted Flash memory from ROM mode.
  • Page 8: Mechanical Dimension

    MECHANICAL DIMENSION Symbol Dimension (mm) 17.00 22.00 3.85 1.05 1.90 1.10 0.80 1.50 3.65 3.25 2.10 1.10...
  • Page 9: Electrical Specifications

    ELECTRICAL SPECIFICATIONS ABSOLUTE MAXIMUM RATINGS Parameter Minimum Maximum Condition Supply Voltage (VCC) -0.5 Volt Backup Battery Voltage (V_BCKP) -0.5 Volt Input Pin Voltage -0.5 VCC+0.5 Volt Input Power at RF_IN Storage Temperature +100 degC OPERATING CONDITIONS Parameter Unit Supply Voltage (VDD33) Volt Acquisition Current (exclude active antenna current) Tracking Current (exclude active antenna current)
  • Page 10: Application Circuit

    APPLICATION CIRCUIT...
  • Page 11 ODOMETER and DIRECTION pins. When changing between ADR and ODR mode of operation, cold start command should be issued, or the V_BCKP power should be removed such that internal DR state will be cleared and PX1175RDP will re-do DR calibration. CALIBRATION of DR PX1175RDP performs calibration of gyro bias and odometer scale automatically using GNSS.
  • Page 12: Antenna Considerations

    RTK performance. POWER SUPPLY REQUIREMENT PX1175RDP requires a stable power supply, avoid ripple on VCC pin (<50mVpp). Power supply noise can affect the receiver’s sensitivity. Bypass capacitors should be placed close to the module VCC pin, with values adjusted depending on the amount and type of noise present on the supply line.
  • Page 13: 1Pps Output

    HANDLING GUIDELINE The PX1175RDP modules are rated MSL4, must be used for SMT reflow mounting within 72 hours after taken out from the vacuumed ESD-protective moisture barrier bag in factory condition < 30degC / 60% RH. If this floor life time is exceeded, or if the received ESD-protective moisture barrier bag is not in vacuumed state, then the device need to be pre-baked before SMT reflow process.
  • Page 14 RTK Usage Guideline Below conditions are required for getting RTK fix solution. If the conditions are not met, PX1175RDP will only have float or DGPS/3D solution and behave like a normal GNSS receiver. * Base and rover distance under 30Km...
  • Page 15 “*” Checksum delimiter. Checksum field. <CR><LF> 0D0A Ending of sentence. (carriage return, line feed) Table 2: Overview of SkyTraq receiver’s NMEA messages $GPGGA Time, position, and fix related data of the receiver. $GNGLL Position, time and fix status. $GNGSA Used to represent the ID’s of satellites which are used for position fix. When GPS satellites are used for position fix, $GNGSA sentence is output with system ID 1.
  • Page 16 The formats of the supported NMEA messages are described as follows: GGA – Global Positioning System Fix Data Time, position and fix related data for a GPS receiver. Structure: $GPGGA,hhmmss.sss,ddmm.mmmmmmm,a,dddmm.mmmmmmm,a,x,xx,x.x,x.x,M,x.x,M,x.x,xxxx*hh<CR><LF> 5 6 7 8 9 11 12 Example: $GPGGA,072120.000,2447.0913289,N,12100.5212111,E,4,27,0.5,94.715,M,19.600,M,2.000,0000*49<CR><LF> Field Name Example Description...
  • Page 17 GLL – Latitude/Longitude Latitude and longitude of current position, time, and status. Structure: $GNGLL,ddmm.mmmmmmm,a,dddmm.mmmmmmm,a,hhmmss.sss,A,a*hh<CR><LF> 6 7 8 Example: $GNGLL,2447.0913289,N,12100.5212111,E,072120.000,A,D*4E<CR><LF> Field Name Example Description Latitude 2447.0913289 Latitude in ddmm.mmmmmmm format Leading zeros transmitted N/S Indicator Latitude hemisphere indicator ‘N’ = North ‘S’...
  • Page 18 GSA – GNSS DOP and Active Satellites GNSS receiver operating mode, satellites used in the navigation solution reported by the GGA or GNS sentence and DOP values. Structure: $GNGSA,A,x,xx,xx,xx,xx,xx,xx,xx,xx,xx,xx,xx,xx,x.x,x.x,x.x,x*hh<CR><LF> 1 2 3 3 3 3 3 3 3 3 3 3 3 3 4 5 6 7 8 Example: $GNGSA,A,3,02,05,06,12,13,19,20,193,195,199,,,1.0,0.5,0.9,1*01<CR><LF>...
  • Page 19 *GNSS Signal ID identifies the GNSS signal name according to Table 3. Table 3: GNSS Identification Table for GSA, GSV System System ID (Talker) Signal ID Signal Name 1 (GP) All signals L1 C/A L1 P(Y) L2 P(Y) L2C-M L2C-L L5-I L5-Q GLONASS...
  • Page 20 GSV – GNSS Satellites in View Number of satellites (SV) in view, satellite ID numbers, elevation, azimuth, and SNR value. Four satellites maximum per transmission. Structure: $GPGSV,x,x,xx,xx,xx,xxx,xx,…,xx,xx,xxx,xx,x *hh<CR><LF> 1 2 3 4 5 6 7 4 5 6 7 8 9 Example: $GPGSV,3,1,11,195,73,125,46,193,71,078,46,199,60,166,41,02,56,002,46,1*59<CR><LF>...
  • Page 21 Time, date, position, course and speed data provided by a GNSS navigation receiver. Structure: $GPRMC,hhmmss.sss,A,dddmm.mmmmmmm,a,dddmm.mmmmmmm,a,x.x,x.x,ddmmyy,,,a,a*hh<CR><LF> 6 7 8 10 11 12 Example: $GNRMC,072120.000,A,2447.0913289,N,12100.5212111,E,000.0,000.0,050721,,,R,V*14<CR><LF> Field Name Example Description UTC time 072120.000 UTC time in hhmmss.sss format (000000.00 ~ 235959.999) Status Status ‘V’...
  • Page 22 Structure: GPVTG,x.x,T,,M,x.x,N,x.x,K,a*hh<CR><LF> Example: $GNVTG,000.0,T,,M,000.0,N,000.0,K,D*16<CR><LF> Field Name Example Description Course 000.0 True course over ground in degrees (000.0 ~ 359.9) Speed 000.0 Speed over ground in knots (000.0 ~ 999.9) Speed 000.0 Speed over ground in kilometers per hour (000.0 ~ 1800.0) Mode Mode indicator ‘A’...
  • Page 23 STI,20 Dead Reckoning Status message Structure: PSTI,xx,x,x,x,xx,x,x,x,xxx.xx,xx.xx,xx.xx,x.xx*xx<CR><LF> 1 2 3 4 5 6 7 8 11 12 13 Example: $PSTI,20,1,1,1,5,A,0,0,-58.48,20.14,0.01,1.01*73<CR><LF> Field Example Format Unit Description numeric Proprietary message identifier: 20 numeric DR Calibration Status 1: calibrated 0: not calibrated numeric Gyro Calibrate Status 1: calibrated 0: not calibrated...
  • Page 24: Ordering Information

    ORDERING INFORMATION Model Name Description PX1175RDP GNSS RTK Dead Reckoning receiver module with barometric pressure sensor for superior altitude sensing performance...
  • Page 25 Revision History Revision Date Description July 11, 2023 Initial release The information provided is believed to be accurate and reliable. These materials are provided to customers and may be used for informational purposes only. No responsibility is assumed for errors or omissions in these materials, or for its use. Changes to specification can occur at any time without notice.

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