background image

JP14-R-LP & JP14-Q-LP F

ALCOM

 GPS R

ECEIVERS

V

ERSION

 1.0.0

but the navigation solution still needs to be computed, thus consuming power is 
less than in the full power state.

Standby state

In the standby state, power remains applied to the JP14 family, but the RF section 
is completely powered off and the clock to the baseband is stopped. About 600 
µA of current is drawn in this state for the internal core regulator, RTC and battery-
backed   RAM.   The   receiver   enters   this   state   when   a   position   fix   has   been 
computed and reported. Typically, before shutting down the RTC wakeup register 
is programmed to wake up the system sometime in the future. 

Remark

:  The environment temperature may also affect the power consumption in the Standby state.

Figure 4:

Three system states into the ATP mode.

The transition from Standby state back to the full power is generated through the 
internal RTC, which transmits a wake up signal to the GPS engine to switch it on. The 
JP14 is woken up and begins to acquire the on view satellites and to collect their 
data.  Under normal  tracking conditions, the  receiver  is set  for  a specific update 
period (range  from  1  to  10 seconds), and a specific sampling time during each 
period (range  from  200 to  900 ms). The  receiver  turns  to  full power state  for  the 
sampling time to collect data, and then operates in Standby state for the remainder 
of the update period. The next full-power state is initiated by an RTC wakeup. But in 
harsh tracking environments the receiver automatically switches to full power state 
to improve navigation performance. When the satellites are sorted according their 
signal strength, the fourth satellite determines if the transition will occur or not. The 
threshold   is   26   dB-Hz.   When   tracking,   conditions   return   to   normal   (four   or   more 
satellites with C/No of 30 dB-Hz or higher), the receiver switches back to the power 
saving mode.  

5.4.3 Push-to-Fix Mode 

 

 

The Push-to-Fix mode puts the FALCOM JP14 family into a background duty cycle 
which provides a periodic refresh of position, receiver time, ephemeris data and RTC 
calibration every 10 seconds to 2 hours.  The transition of receiver into the Push-to-Fix 
mode  can   be   implemented   and  configured  by   using  either   the  

Action│Set   Low 

Power (Trickle Power) …

  command available in SiRFDemo evaluation software or 

the input command described in chapter 

5.4.4

 on page 

17

The PTF period is 30 minutes by default but can be anywhere between 10 seconds 
and 2 hours. When the PTF mode is enabled, due to a new PTF cycle, the receiver 

This confidential document is the property of FALCOM  and may not be copied or circulated without permission.

Page 16

Содержание JP14-Q-LP

Страница 1: ...THIS DOCUMENT IS AVAILABLE AT HTTP WWW FALCOM DE JP14 R LP JP14 Q LP GPS Receivers Lead free products Hardware description Version 1 0 0 Created Monday 25 February 2008...

Страница 2: ...DGPS Accuracy 13 5 3 1 4 Datum 13 5 3 1 5 Time to First Position 13 5 3 1 6 Sensitivity 14 5 3 1 7 Dynamic Conditions 14 5 3 1 8 DC Power 14 5 3 1 9 Serial Port 14 5 3 1 10 Time 1PPS Pulse 14 5 4 Pow...

Страница 3: ...essages 24 7 2 3 Transport Message 25 8 MECHANICAL DRAW 26 9 LAYOUT RECOMMENDATION 29 9 1 Ground planes 29 9 2 RF connection 29 9 3 Soldering profile 30 10 FIRST STEPS TO MAKE IT WORK 31 11 APPENDIX 3...

Страница 4: ...on history This table provides a summary of the document revisions Version Author Changes Release date 1 0 0 F Beqiri Initial version 25 02 2008 This confidential document is the property of FALCOM an...

Страница 5: ...de Trademarks Some mentioned products are registered trademarks of their respective companies Copyright This document is copyrighted by FALCOM WIRELESS COMMUNICATIONS GmbH with all rights reserved No...

Страница 6: ...ch unit has an integrated temperature compensated crystal oscillator TCXO Due to the higher stability of frequency they offer a high improved GPS performance In addition higher sensitivity allows them...

Страница 7: ...breviations Abbreviation Description A GPS Assisted Global Positioning System BGA Ball Grid Array DGPS Differential GPS DOP Dilution of Precision GPS Global Positioning System GGA GPS Fixed Data LNA L...

Страница 8: ...uit Board PRN Pseudo random noise IF Intermediate Frequency A D Analog Digital 1 3 Related documents 1 SiRF binary and NMEA protocol specification www falcom de Support Documentation Sirf SiRFmessages...

Страница 9: ...s The GPS receiver consists of many small parts which can come loose and could be swallowed by small children Thoughtless handling can damage the GPS receiver 2 4 Operation antenna Operate the GPS rec...

Страница 10: ...ns for the protection of public exposure to RF electromagnetic energy established by government bodies and professional organizations such as directives of the European Community Directorate General V...

Страница 11: ...p 4 Mbit FLASH and 1 Mbit SRAM Operating voltage 3 3 V DC 5 Power consumption 140 mW continuous mode Power management Adaptive TricklePower ATP Push to Fix PTF For more details see chapter 5 4 Tempera...

Страница 12: ...y make the JP14 R LP Q LP highly efficient engines for wide variety of location applications The core of JP14 R LP Q LP contains a built in sequencer which handles all the high rate interrupts for GPS...

Страница 13: ...6 12 5 25 and 49 MHz Data bus 16 bit 5 3 1 2 Accuracy Position Autonomous 10 meters CEP without SA SBAS 5 meter Velocity 0 1 meters second without SA Time 1 microsecond synchronized to GPS time 5 3 1...

Страница 14: ...1000 knots max Acceleration 4 g max Jerk 20 meters second max 5 3 1 8 DC Power Main power 3 3 V DC 5 Core power 1 5 V DC Continuous mode approx 45 mA at 3 3 V DC with an active antenna FAL ANT 3 Backu...

Страница 15: ...l be needed on the next power up scenario 5 4 2 Adaptive TricklePower mode ATP Adaptive TricklePower ATP is a variant of TricklePower But only ATP and Push To Fix PTF is described in next chapter mode...

Страница 16: ...to 900 ms The receiver turns to full power state for the sampling time to collect data and then operates in Standby state for the remainder of the update period The next full power state is initiated...

Страница 17: ...messages to the target unit refer to chapter Appendix section 11 1 page 33 Syntax PSRF107 Mode OnTimeMs LPInterval MaxAcqTimeMs MaxOffTimeMs TPAdaptive CS CR LF Examples PSRF107 1 400 2000 60000 6000...

Страница 18: ...target receiver should remain off sleep mode before making another attempt to navigate This mode is enabled if the target receiver is turned on and acquires satellites but does not navigate This mode...

Страница 19: ...n 13 NC Not connected 14 NC 15 NC 16 GPIO0 I O General propose input output CMOS 17 NC Not connected 18 GND Digital ground 0 V 19 GND_RF Analogue ground 20 VANT I Power supply for an active antenna Up...

Страница 20: ...t for baseband processor Do not use leave it open CMOS 10 PWRCTL O Control outputs Do not use leave it open CMOS 11 BOOTSEL I Boots the unit into the Update mode if it is set to HIGH CMOS VCC 12 WAKEU...

Страница 21: ...t this Pin to high 3 3 V DC for reprogramming the flash of the JP14 R LP Q LP for instance updating a new firmware for the JP14 R LP Q LP 6 4 Serial communication signals The board supports two full d...

Страница 22: ...a bias for an external active antenna can be provided in two ways to pin VANT In order to use a 5 V or 12 V active GPS antenna the VANT has to be connected to 5 V 12 V external power supply respective...

Страница 23: ...E 30 Nav Lib SV State Data Satellite State Data 0 x 1F 31 Nav Lib Initialization Data Initialization Data 0 x FF 255 Development Data Various status messages Table 6 SiRF Output Messages Table 7 lists...

Страница 24: ...umbers elevation azimuth and SNR values MSS This message can be switched on via SiRFdemo software Signal to noise ratio signal strength frequency and bit rate from a radio beacon receiver RMC Time dat...

Страница 25: ...m the example strings but must be sent to terminate the message and cause the receiver to process that input message CheckSum The checksum is 15 bit checksum of the bytes in the payload data The follo...

Страница 26: ...L The absolute maximum dimension of the modules are JP14 R 10 2 mm x 24 5 mm B x L and JP14 Q 15 7 mm x 17 2 mm B x L Figures 6 and 7 show the top view of the JP14 R LP Q LP GPS receivers and provide...

Страница 27: ...soldering Figure 8 shows the bottom view on JP14 R and provides an overview of the mechanical dimensions of the pointed balls Figure 8 The mechanical draw of the JP14 R This confidential document is...

Страница 28: ...hows the bottom view on JP14 Q and provides an overview of the mechanical dimensions of the pointed balls Figure 9 The mechanical draw of the JP14 Q This confidential document is the property of FALCO...

Страница 29: ...re 10 Digital GND Analog GND connected internally Figure 10 Ground plane of the JP14 R LP Q LP GPS receivers 9 2 RF connection The JP14 R LP Q LP GPS receivers are designed to be functional by using e...

Страница 30: ...is a reference to the soldering machine FALCOM utilizes This profile can vary by using different paste types and soldering machines and it should be adapted to the customer application NO liability is...

Страница 31: ...ines which supply the VCC pin to 3 3 V properly If they are correctly connected the board is full powered and the unit begins obtaining its position fix Serial Interface The JP14 family provides two s...

Страница 32: ...Evaluation board with connected JP14 R LP Q LP GPS receiver The GPS Evaluation Kit contains Evaluation Box JP14 sample with soldered antenna cable power supply AC DC adapter Type FW738 05 Output 5VDC...

Страница 33: ...o do this open Action menu from main window and start Transmit Serial Message On the appeared dialog box select NMEA protocol from the Protocol Wrapper option and type the following command onto the m...

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