Microsoft Word - MC-1613_datasheet_v1.x.doc

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Product name Description Version MC-1613 Datasheet of MC-1613 stand-alone GPS module 1.3 1 Introduction LOCOSYS GPS MC-1613 module features high sensitivity, low power and ultra small form factor.

1 Product name Description Version MC-1613 Datasheet of MC-1613 stand-alone GPS module Introduction LOCOSYS GPS MC-1613 module features high sensitivity, low power and ultra small form factor. This GPS module is powered by MediaTek, it can provide you with superior sensitivity and performance even in urban canyon and dense foliage environment. This module supports hybrid ephemeris prediction to achieve faster cold start. One is self-generated ephemeris prediction that is no need of both network assistance and host CPU s intervention. This is valid for up to 3 days and updates automatically from time to time when GPS module is powered on and satellites are available. The other is server-generated ephemeris prediction that gets from an internet server. This is valid for up to 14 days. Both ephemeris predictions are stored in the on-board flash memory and perform a cold start time less than 15 seconds. 2 Features MediaTek high sensitivity solution Support 66-channel GPS Low power consumption Fast TTFF at low signal level Built-in 12 multi-tone active interference canceller Free hybrid ephemeris prediction to achieve faster cold start Built-in data logger Up to 10 Hz update rate Capable of SBAS (WAAS, EGNOS, MSAS, GAGAN) Support SBAS ranging Support Japan QZSS Indoor and outdoor multi-path detection and compensation Small form factor 15.9 x 13.1 x 2.2 mm SMD type with stamp holes; RoHS compliant 3 Application Personal positioning and navigation Automotive navigation Marine navigation 2010 Page 1/17

2 Fig 3-1 System block diagram. GPS active antenna 3.3V TX RX VCC LNA Impedance 50 ohm 2~4.3V Battery keep alive to get hot start and AGPS start LDO output 3.3V 1 RFIN V_BCKP VCC MC PPS 19 Micro processor Fig 3-2 Typical application circuit that uses an active antenna 2010 Page 2/17

3 3.3V GPS passive antenna TX RX VCC Impedance 50 ohm 2~4.3V Battery keep alive to get hot start and AGPS start LDO output 3.3V 1 RFIN V_BCKP VCC RX 30 TX /RESET MC PPS 19 Micro processor Fig 3-3 Typical application circuit that uses a passive antenna Page 3/17

4 4 GPS receiver and antenna 4.1 GPS receiver Chip Frequency Channels Update rate Sensitivity Acquisition Time Position Accuracy Max. Altitude Max. Velocity MediaTek MT3339 L MHz, C/A code Support 66 channels (22 Tracking, 66 Acquisition) 1Hz default, up to 10Hz Tracking Cold start Hot start (Open Sky) Hot start (Indoor) Cold Start (Open Sky) Autonomous SBAS < 50,000 m < 515 m/s Protocol Support NMEA 0183 ver 3.01 up to -165dBm (with external LNA) up to -148dBm (with external LNA) < 1s (typical) < 30s 32s (typical) without AGPS < 15s (typical) with AGPS (hybrid ephemeris prediction) 3m (2D RMS). 2.5m (depends on accuracy of correction data) bps (1), 8 data bits, no parity, 1 stop bits (default) 1Hz: GGA, GLL, GSA, GSV, RMC, VTG Note 1: Both baud rate and output message rate are configurable to be factory default. 5 Software interface 5.1 NMEA output message Table NMEA output message NMEA record GGA GLL GSA GSV RMC VTG Description Global positioning system fixed data Geographic position - latitude/longitude GNSS DOP and active satellites GNSS satellites in view Recommended minimum specific GNSS data Course over ground and ground speed GGA--- Global Positioning System Fixed Data Table contains the values for the following example: $GPGGA, , ,N, ,E,1,08,1.1,63.8,M,15.2,M,,0000*64 Table5.1-2 GGA Data Format Name Example Units Description Message ID $GPGGA GGA protocol header 2010 Page 4/17

5 UTC Time hhmmss.sss Latitude ddmm.mmmm N/S indicator N N=north or S=south Longitude dddmm.mmmm E/W Indicator E E=east or W=west Position Fix Indicator 1 See Table Satellites Used 08 Range 0 to 12 HDOP 1.1 Horizontal Dilution of Precision MSL Altitude 63.8 mters Units M mters Geoid Separation 15.2 mters Units M mters Age of Diff. Corr. second Null fields when DGPS is not used Diff. Ref. Station ID 0000 Checksum *64 <CR> <LF> End of message termination Table Position Fix Indicators Value Description 0 Fix not available or invalid 1 GPS SPS Mode, fix valid 2 Differential GPS, SPS Mode, fix valid 3-5 Not supported 6 Dead Reckoning Mode, fix valid GLL--- Geographic Position Latitude/Longitude Table contains the values for the following example: $GPGLL, ,N, ,E, ,A,A*52 Table GLL Data Format Name Example Units Description Message ID $GPGLL GLL protocol header Latitude ddmm.mmmm N/S indicator N N=north or S=south Longitude dddmm.mmmm E/W indicator E E=east or W=west UTC Time hhmmss.sss Status A A=data valid or V=data not valid 2010 Page 5/17

6 Mode A A=autonomous, D=DGPS, E=DR, N=Data not valid, R=Coarse Position (1), S=Simulator Checksum *52 <CR> <LF> End of message termination GSA---GNSS DOP and Active Satellites Table contains the values for the following example: $GPGSA,A,3,24,07,17,11,28,08,20,04,,,,,2.0,1.1,1.7*35 Table GSA Data Format Name Example Units Description Message ID $GPGSA GSA protocol header Mode 1 A See Table Mode 2 3 See Table ID of satellite used 24 Sv on Channel 1 ID of satellite used 07 Sv on Channel 2.. ID of satellite used Sv on Channel 12 PDOP 2.0 Position Dilution of Precision HDOP 1.1 Horizontal Dilution of Precision VDOP 1.7 Vertical Dilution of Precision Checksum *35 <CR> <LF> End of message termination Table Mode 1 Value M A Description Manual- forced to operate in 2D or 3D mode Automatic-allowed to automatically switch 2D/3D Table Mode 2 Value Description 1 Fix not available 2 2D 3 3D GSV---GNSS Satellites in View Table contains the values for the following example: $GPGSV,3,1,12,28,81,285,42,24,67,302,46,31,54,354,,20,51,077,46*73 $GPGSV,3,2,12,17,41,328,45,07,32,315,45,04,31,250,40,11,25,046,41*75 $GPGSV,3,3,12,08,22,214,38,27,08,190,16,19,05,092,33,23,04,127,*7B 2010 Page 6/17

7 Table GSV Data Format Name Example Units Description Message ID $GPGSV GSV protocol header Total number of messages 1 3 Range 1 to 3 Message number 1 1 Range 1 to 3 Satellites in view 12 Satellite ID 28 Channel 1 (Range 01 to 196) Elevation 81 degrees Channel 1 (Range 00 to 90) Azimuth 285 degrees Channel 1 (Range 000 to 359) SNR (C/No) 42 db-hz Channel 1 (Range 00 to 99, null when not tracking) Satellite ID 20 Channel 4 (Range 01 to 196) Elevation 51 degrees Channel 4 (Range 00 to 90) Azimuth 077 degrees Channel 4 (Range 000 to 359) SNR (C/No) 46 db-hz Channel 4 (Range 00 to 99, null when not tracking) Checksum *73 <CR> <LF> End of message termination 1. Depending on the number of satellites tracked multiple messages of GSV data may be required. RMC---Recommended Minimum Specific GNSS Data Table contains the values for the following example: $GPRMC, ,A, ,N, ,E,2.69,79.65,100106,,,A*53 Table RMC Data Format Name Example Units Description Message ID $GPRMC RMC protocol header UTC Time hhmmss.sss Status A A=data valid or V=data not valid Latitude ddmm.mmmm N/S Indicator N N=north or S=south Longitude dddmm.mmmm E/W Indicator E E=east or W=west Speed over ground 2.69 knots True Course over ground degrees Date ddmmyy Magnetic variation Variation sense Mode A degrees E=east or W=west (Not shown) A=autonomous, D=DGPS, E=DR, N=Data not valid, R=Coarse Position, S=Simulator 2010 Page 7/17

8 Checksum *53 <CR> <LF> End of message termination VTG---Course Over Ground and Ground Speed Table contains the values for the following example: $GPVTG,79.65,T,,M,2.69,N,5.0,K,A*38 Table VTG Data Format Name Example Units Description Message ID $GPVTG VTG protocol header Course over ground degrees Measured heading Reference T True Course over ground degrees Measured heading Reference M Magnetic Speed over ground 2.69 knots Measured speed Units N Knots Speed over ground 5.0 km/hr Measured speed Units K Kilometer per hour Mode A A=autonomous, D=DGPS, E=DR, N=Data not valid, R=Coarse Position (1), S=Simulator Checksum *38 <CR> <LF> End of message termination 5.2 Proprietary NMEA input/output message Please refer to MTK proprietary message. 5.3 Examples to configure the power mode of GPS module The GPS module supports different power modes that user can configure by issuing software commands Standby mode User can issue software command to make GPS module go into standby mode that consumes less than 200uA current. GPS module will be awaked when receiving any byte. The following flow chart is an example to make GPS module go into standby mode and then wake up Page 8/17

9 Start GPS module is powered on and in normal operation mode Change GPS to standby mode unsigned char StandbyMode[] = {"$PMTK161,0*28\x0D\x0A"}; Wake up GPS module Yes No Issue any byte to wake up GPS module GPS module will return {"$PMTK010,002*2D\x0D\x0A"} and start normal operation. End Periodic mode When GPS module is commanded to periodic mode, it will be in operation and standby periodically. Its status of power consumption is as below chart. The following flow chart is an example to make GPS module go into periodic mode 2010 Page 9/17

10 and then back to normal operation mode. Start GPS module is powered on Change GPS to periodic mode with 3000ms on and 12000ms standby if position fix is available, otherwise (18000, 72000) ms will be applied. Set GPS to normal operation mode? unsigned char PeriodicMode[] = {"$PMTK225,2,3000,12000,18000,72000*15\x0D\x0A"}; Note: minimum on time is 2000ms. maximum standby time is ms (6 days) Yes GPS module will return message "$PMTK001,225,3*35\x0D\x0A" if command is accepted. GPS is in standby now Yes Issue any byte to GPS and wait it awake No End GPS is in periodic mode No Issue command of normal operation mode End GPS is in normal mode unsigned char NormalMode[] = {"$PMTK225,0*2B\x0D\x0A"}; GPS module will return message "$PMTK001,225,3*35\x0D\x0A" if command is accepted AlwaysLocate TM mode AlwaysLocate TM is an intelligent controller of periodic mode. Depending on the environment and motion conditions, GPS module can adaptively adjust working/standby time to achieve balance of positioning accuracy and power consumption. In this mode, the host CPU does not need to control GPS module until the host CPU needs the GPS position data. The following flow chart is an example to make GPS module go into AlwaysLocate Tm mode and then back to normal operation mode Page 10/17

11 Note: AlwaysLocate TM is a trade mark of MTK. Start GPS module is powered on Change GPS to AlwaysLocate mode unsigned char AlwaysLocateMode[] = {"$PMTK225,8*23\x0D\x0A"}; GPS module will return message "$PMTK001,225,3*35\x0D\x0A" if command is accepted. Yes Request a GPS position data Yes No No Issue any byte to get GPS position data Set GPS to normal operation mode? Yes Issue any byte to GPS and wait it awake Change GPS back to AlwaysLocate mode No Set GPS to normal operation mode unsigned char NormalMode[] = {"$PMTK225,0*2B\x0D\x0A"}; End GPS is in normal mode 5.4 Data logger The GPS module has internal flash memory for logging GPS data. The configurations 2010 Page 11/17

12 include time interval, distance, speed, logging mode, and etc. For more information, please contact us. 6 Pin assignment and descriptions Table 6-1 Pin descriptions Pin # Name Type Description Note 1 RFIN I GPS RF signal input 1 2 P Ground 3 Not connected 4 Not connected 5 V_BCKP P Backup battery supply voltage This pin must be powered to enable the module. 2 6 P Ground 7 Not connected 8 Not connected 9 Not connected 10 Not connected 11 VCC P DC supply voltage Page 12/

13 12 Not connected 13 /RESET I Reset input, active low. GPS module has internal power-on reset circuit, user can leave this pin floating. 14 Not connected 15 P Ground 16 Not connected 17 Not connected 18 Not connected 19 Not connected 20 1PPS O Pulse per second (default 100ms pulse/sec) 21 Not connected 22 Not connected 23 Not connected 24 P Ground 25 Not connected 26 Not connected 27 Not connected 28 Not connected 29 Not connected 30 TX O Serial output (Default NMEA) 31 RX I Serial input (Default NMEA) 32 Not connected 33 P Ground 34 Not connected 35 Not connected 36 P Ground <Note> 1. RFIN does not have short circuit protection. 2. In order to get AGPS (Long Term Orbit) advantage, this pin must be always powered during the period of effective AGPS Page 13/17

14 7 DC & Temperature characteristics 7.1 Absolute maximum ratings Parameter Symbol Ratings Units Input Voltage VCC 4.3 V Input Backup Battery Voltage V_BCKP 4.3 V Operating Temperature Range Topr -40 ~ 85 Storage Temperature Range Tstg -40 ~ DC Electrical characteristics Parameter Symbol Conditions Min. Typ. Max. Units Input Voltage VCC V Input Backup Battery Voltage V_BCKP V VCC = 3.3V, w/o active antenna, Supply Current Iss Peak Acquisition Tracking Standby 87 (1) ma 26 ma 18 (2) ma 170 ua Backup Battery Current Ibat VCC = 0V 6 ua High Level Input Voltage VI H V Low Level Input Voltage VI L V High Level Input Current I I H no pull-up or down -1 1 ua Low Level Input Current I I L no pull-up or down -1 1 ua High Level Output Voltage VOH 2.4 V Low Level Output Voltage VOL 0.4 V High Level Output Current IOH 2 ma Low Level Output Current IOL 2 ma Note 1. This happens when downloading AGPS data to MC Note 2. Measured when position fix (1Hz) is available, input voltage is 3.3V and the function of self-generated ephemeris prediction is inactive. 7.3 Temperature characteristics Parameter Symbol Min. Typ. Max. Units Operating Temperature Topr Storage Temperature Tstg Page 14/17

15 8 Mechanical specification 8.1 Outline dimensions 8.2 Recommended land pattern dimensions 2010 Page 15/17

16 9 Reel packing information 2010 Page 16/17

17 Document change list Revision 1.0 First release on Dec. 24, Revision 1.0 to Revision 1.1 (April 11, 2011) Upgraded GPS firmware to version AXN1.5. Changed cold start time from 35s to 33s on page 3 Changed full cold start time from 38s to 34s on page 3 Revised RFIN (pin11) to RFIN (pin1) on page 3. Changed default 1PPS as 100ms pulse/sec on page 10 Revision 1.1 to Revision 1.2 (November 21, 2011) Changed GPS chip from MT3329 to MT3339 on page 4. The units with a capital T after the date code on the metal shield have been changed to new chip. Added the description of hybrid ephemeris prediction in section 1. Added several new features in section 2. Changed Fig 3-1 and Fig 3-2 Added Fig 3-3 Changed hot start time from < 2s to < 1s on page 5. Changed cold start time from 33s to 32s on page 5. Changed Max. Altitude from 18,000m to 50,000m on page 5. Removed the section 4.2 Changed the range of satellite ID in GSV message from 32 to 196 on page 7. Added N = data not valid, R=Coarse Position, S=Simulator in GLL, RMC and VTG message. Added section 5.3 and 5.4 Changed the maximum input voltage of VCC from 3.6V to 4.3V in the section 7.2. Changed the peak supply current from 160mA to 87mA in the section 7.2. Changed the acquisition current from 35mA to 26mA in the section 7.2. Changed the tracking current from 33mA to 18mA in the section 7.2. Added standby current, 170uA in the section 7.2. Changed the minimum operation temperature from -30 to -40 in the section 7.3 Revision 1.2 to Revision 1.3 (June 24, 2013) Changed tolerance from 15.9±0.15 to 15.9±0.2 on page Page 17/17

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