JN3 Product Description
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JN3 Product Description
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APPLICABILITY TABLE
PRODUCT
JN3
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SPECIFICATIONS SUBJECT TO CHANGE WITHOUT NOTICE
Notice
While reasonable efforts have been made to assure the accuracy of this document, Telit
assumes no liability resulting from any inaccuracies or omissions in this document, or from
use of the information obtained herein. The information in this document has been carefully
checked and is believed to be entirely reliable. However, no responsibility is assumed for
inaccuracies or omissions. Telit reserves the right to make changes to any products described
herein and reserves the right to revise this document and to make changes from time to time
in content hereof with no obligation to notify any person of revisions or changes. Telit does
not assume any liability arising out of the application or use of any product, software, or
circuit described herein; neither does it convey license under its patent rights or the rights of
others.
It is possible that this publication may contain references to, or information about Telit
products (machines and programs), programming, or services that are not announced in your
country. Such references or information must not be construed to mean that Telit intends to
announce such Telit products, programming, or services in your country.
Copyrights
This instruction manual and the Telit products described in this instruction manual may be,
include or describe copyrighted Telit material, such as computer programs stored in
semiconductor memories or other media. Laws in the Italy and other countries preserve for
Telit and its licensors certain exclusive rights for copyrighted material, including the
exclusive right to copy, reproduce in any form, distribute and make derivative works of the
copyrighted material. Accordingly, any copyrighted material of Telit and its licensors
contained herein or in the Telit products described in this instruction manual may not be
copied, reproduced, distributed, merged or modified in any manner without the express
written permission of Telit. Furthermore, the purchase of Telit products shall not be deemed
to grant either directly or by implication, estoppel, or otherwise, any license under the
copyrights, patents or patent applications of Telit, as arises by operation of law in the sale of a
product.
Computer Software Copyrights
The Telit and 3rd Party supplied Software (SW) products described in this instruction manual
may include copyrighted Telit and other 3rd Party supplied computer programs stored in
semiconductor memories or other media. Laws in the Italy and other countries preserve for
Telit and other 3rd Party supplied SW certain exclusive rights for copyrighted computer
programs, including the exclusive right to copy or reproduce in any form the copyrighted
computer program. Accordingly, any copyrighted Telit or other 3rd Party supplied SW
computer programs contained in the Telit products described in this instruction manual may
not be copied (reverse engineered) or reproduced in any manner without the express written
permission of Telit or the 3rd Party SW supplier. Furthermore, the purchase of Telit products
shall not be deemed to grant either directly or by implication, estoppel, or otherwise, any
license under the copyrights, patents or patent applications of Telit or other 3rd Party supplied
SW, except for the normal non-exclusive, royalty free license to use that arises by operation
of law in the sale of a product.
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Usage and Disclosure Restrictions
License Agreements
The software described in this document is the property of Telit and its licensors. It is
furnished by express license agreement only and may be used only in accordance with the
terms of such an agreement.
Copyrighted Materials
Software and documentation are copyrighted materials. Making unauthorized copies is
prohibited by law. No part of the software or documentation may be reproduced, transmitted,
transcribed, stored in a retrieval system, or translated into any language or computer language,
in any form or by any means, without prior written permission of Telit
High Risk Materials
Components, units, or third-party products used in the product described herein are NOT
fault-tolerant and are NOT designed, manufactured, or intended for use as on-line control
equipment in the following hazardous environments requiring fail-safe controls: the operation
of Nuclear Facilities, Aircraft Navigation or Aircraft Communication Systems, Air Traffic
Control, Life Support, or Weapons Systems (High Risk Activities"). Telit and its supplier(s)
specifically disclaim any expressed or implied warranty of fitness for such High Risk
Activities.
Trademarks
TELIT and the Stylized T Logo are registered in Trademark Office. All other product or
service names are the property of their respective owners.
Copyright © Telit Communications S.p.A. 2015.
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Contents
1. Introduction .................................................................................................................................. 8
1.1. Scope ....................................................................................................................................... 8
1.2. Audience .................................................................................................................................. 8
1.3. Contact Information, Support .................................................................................................. 8
1.4. Document Organization .......................................................................................................... 9
1.5. Text Conventions .................................................................................................................... 9
1.6. Related Documents ............................................................................................................... 10
2. General Product Description ..................................................................................................... 11
3. Technical Description ................................................................................................................. 12
3.1. Product Compatibility ........................................................................................................... 12
3.2. Receiver Architecture ............................................................................................................ 13
3.3. Major Components ................................................................................................................ 13
3.3.1. GSD4e Chip ............................................................................................................................... 13
3.3.2. RF_IN ........................................................................................................................................ 14
3.3.3. VCC_IN ..................................................................................................................................... 14
3.3.4. VBATT ...................................................................................................................................... 14
3.3.5. Host Port .................................................................................................................................... 14
3.3.6. MEMS Sensor Interface ............................................................................................................. 14
3.3.7. SAW Filter (1.575 GHz) ............................................................................................................ 14
3.3.8. TCXO ......................................................................................................................................... 14
3.3.9. RTC ............................................................................................................................................ 14
3.3.10. Memory ...................................................................................................................................... 14
3.4. Physical Characteristics ......................................................................................................... 15
3.5. Mechanical Specification ...................................................................................................... 15
3.6. External Antenna Connection ............................................................................................... 15
3.7. Input/Output and Power Connections ................................................................................... 15
3.8. Environmental ....................................................................................................................... 15
3.9. Compliances .......................................................................................................................... 15
3.10. Marking/Serialization ........................................................................................................ 16
3.11. Active Antenna Gain Requirements .................................................................................. 16
4. Software ....................................................................................................................................... 17
4.1. TTFF (Time to First Fix) ....................................................................................................... 17
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4.1.1. Hot Start ..................................................................................................................................... 17
4.1.2. Warm Start ................................................................................................................................. 17
4.1.3. Cold Start ................................................................................................................................... 17
4.2. AGPS ..................................................................................................................................... 18
4.3. Time Mark Pulse (1PPS) ....................................................................................................... 18
4.4. Power Management ............................................................................................................... 18
4.4.1. Adaptive Trickle Power (ATP) .................................................................................................. 18
4.5. Differential Aiding ................................................................................................................ 18
4.5.1. Satellite Based Augmentation Systems (SBAS) ........................................................................ 18
4.6. 5Hz Update Rate ................................................................................................................... 19
4.7. Dynamic Constraints ............................................................................................................. 19
5. Performance Data ....................................................................................................................... 20
6. Electrical Requirements ............................................................................................................. 21
6.1. Power Supply ........................................................................................................................ 21
6.1.1. VCC_IN ..................................................................................................................................... 21
6.1.2. VBATT ...................................................................................................................................... 21
6.2. External Antenna Voltage ..................................................................................................... 21
6.3. RF (Radio Frequency) Input ................................................................................................. 21
6.4. Antenna Gain ......................................................................................................................... 21
6.5. Burnout Protection ................................................................................................................ 21
6.6. Jamming Performance ........................................................................................................... 21
6.7. Flash Upgradability (Flash only) ........................................................................................... 22
6.8. Patch Updates (EEPROM only) ............................................................................................ 22
6.9. Data Input/Output Specifications .......................................................................................... 22
6.9.1. Voltages and Currents ................................................................................................................ 22
6.9.2. DC Electrical Characteristics ..................................................................................................... 23
6.9.3. Pinout Description...................................................................................................................... 24
7. Software Interface ...................................................................................................................... 25
7.1. NMEA Output Messages ...................................................................................................... 25
7.2. SiRF OSP Output Messages .................................................................................................. 25
7.3. Software Functions and Capabilities ..................................................................................... 26
8. Mechanical Drawing .................................................................................................................. 27
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9. Conformity Assessment.............................................................................................................. 29
9.1. Declaration of Conformity .................................................................................................... 29
9.2. R&TTE Notified Body Opinion ............................................................................................ 30
10. Evaluation Kit ......................................................................................................................... 31
11. Product Handling .................................................................................................................... 32
11.1. Product Packaging and Delivery ....................................................................................... 32
11.2. Moisture Sensitivity ........................................................................................................... 33
11.3. ESD Sensitivity.................................................................................................................. 33
11.4. Safety ................................................................................................................................. 33
11.5. Disposal ............................................................................................................................. 33
12. Ordering Information ............................................................................................................. 34
13. Glossary and Acronyms ......................................................................................................... 35
14. Safety Recommendations ....................................................................................................... 37
15. Document History ................................................................................................................... 38
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1. Introduction
1.1. Scope
Scope of this document is to give an overview of new standalone GPS module JN3.
1.2. Audience
This document is intended for customers developing applications using JN3.
1.3. Contact Information, Support
For general contact, technical support, to report documentation errors and to order
manuals, contact Telit Technical Support Center (TTSC) at:
TS-EMEA@telit.com
TS-NORTHAMERICA@telit.com
TS-LATINAMERICA@telit.com
TS-APAC@telit.com
Alternatively, use:
http://www.telit.com/en/products/technical-support-center/contact.php
For detailed information about where you can buy the Telit modules or for
recommendations on accessories and components visit:
http://www.telit.com
To register for product news and announcements or for product questions contact
Telit Technical Support Center (TTSC).
Our aim is to make this guide as helpful as possible. Keep us informed of your
comments and suggestions for improvements.
Telit appreciates feedback from the users of our information.
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1.4. Document Organization
This document contains the following chapters:
“Chapter 1: “Introduction” provides a scope for this document, target audience,
contact and support information, and text conventions.
“Chapter 2: “General Description” gives an overview of the features of the product.
“Chapter 3: “Technical Description” describes the features of the product.
“Chapter 4: “Software” describes in details the characteristics of the product.
“Chapter 5: “Performance Data” shows the performance information of the product.
“Chapter 6: “Electrical Requirements” describes in details the electrical
characteristics of the product.
“Chapter 7: “Software Interface” provides some fundamental hints about the
conformity assessment that the final application might need.
“Chapter 8: “Mechanical Drawings” provides info about Hardware interfaces.
“Chapter 9: Conformity Assessment provides Declaration of Conformity and
Notified Body Opinions.
“Chapter 10: “Evaluation Kit” provides some fundamental hints about evaluation Kit.
“Chapter 11: “Product Handling” describes the packaging and mounting of the
module.
“Chapter 12: “Ordering Information contains the ordering SKUs for the product
“Chapter 12: “Glossary and acronyms” contain the explanation of acronyms used in
the present document
“Chapter 13: “Safety Recommendation” provides some safety recommendations that
must be follow by the customer in the design of the application that makes use of the
JN3.
“Chapter 14: “Document History” provides the history of the present document.
1.5. Text Conventions
Danger This information MUST be followed or catastrophic equipment failure or
bodily injury may occur.
Caution or Warning Alerts the user to important points about integrating the
module, if these points are not followed, the module and end user equipment may
fail or malfunction.
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Tip or Information Provides advice and suggestions that may be useful when
integrating the module.
All dates are in ISO 8601 format, i.e. YYYY-MM-DD.
1.6. Related Documents
JN3 Hardware User Guide,
JN3 EVK User Guide,
JF2_JN3 Low Power Modes Application Note
JF2_JN3 MEMS Application Note
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2. General Product Description
Building upon the SiRFstarIV™ architecture’s high-performance, the JN3 device incorporates
innovations such as SiRFInstantFix™ and Active Jammer Removal. The JN3 can navigate to
-160dBm and track to -163dBm, providing higher coverage, accuracy and availability. This
next generation Jupiter Module consumes only 13mA (3.3V) in 1-Hz TricklePower™ mode.
The JN3 offers A-GPS support and operate with a 3.3V power supply. JN3 supports a full
range of satellite-based augmentation systems, including WAAS, EGNOS, MSAS and
GAGAN.
The GPS module combines the SiRFstarIV™ GSD4e™ GPS engine, TCXO, SAW filter,
RTC, LDO, level conversion and memory (Flash and EEPROM devices only).
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3. Technical Description
High-speed Location Engine Twice the available DSP memory and search speed of
SiRFstarIII architecture for enhanced sensitivity and navigation performance, greater
coverage, reduced time to fix and improved positional accuracy.
Battery Backup is supported via a separate pin for applications that use a battery backup
source.
MEMS Sensor Interface (I2C DR Port) Static detection is implemented and utilizes an
accelerometer to determine if the module is moving in order to pin position.
Active Jammer Remover Advanced DSP technology actively identifies and removes
jammers prior to correlation. This feature maximizes GPS performance and helps identify
issues during the design phase. Up to 8 jammers can be identified and removed.
5Hz Navigation The JN3 can run with a navigation update rate of 1Hz or 5Hz. This is
controllable in NMEA and OSP mode. Note that the UART baud rate will need to be
increased to support the higher message output (about 38400 baud minimum in NMEA).
High Performance Solution:
- High sensitivity navigation engine (PVT) tracks as low as -163dBm
- 48 track verification channels
- SBAS (WAAS), EGNOS, MSAS, GAGAN
Active Jammer Remover:
- Removes in-band jammers up to 80 dB-Hz
- Tracks up to 8 CW jammers
Advanced Navigation Features:
- Smart sensor I2C interface
- Interrupt input for context change detection
3.1. Product Compatibility
The JN3 incorporates a new technology far advanced compared to the previous SiRFstarIII
designs. It offers an upgrade path from existing Telit and competitive designs.
NMEA version 3.0 protocol is supported as well as the new SiRF ONE SOCKET binary
PROTOCOL (OSP).
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3.2. Receiver Architecture
The functional architecture of the JN3 receiver is shown in Figure 1.
Note: The LNA is included in the GPS chip for passive antenna operation.
Note: LNA is included in the GPS chip for passive antenna operation.
3.3. Major Components
All power supply components are on board including capacitors.
3.3.1. GSD4e Chip
This single chip GPS device includes an integrated Baseband and RF sections. The LNA
amplifies the GPS signal and provides enough gain for the receiver to use a passive antenna.
A very low noise design is utilized to provide maximum sensitivity. This LNA is internal to
the GPS baseband and can be switched between low and high gain mode.
GSD4e
SAW
TCXO
Flash or
EEPROM
VCC_IN
PSU
capacitors
and
inductors
RTC
UART
ACTIVE/PASS
IVE
ANTENNA
POR
1.8V
LDO
VBATT
1PPS
I2C
Level
conversion
Figure 1 JN3 Architecture
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3.3.2. RF_IN
GPS RF signal input. This requires an external BIAS-T and antenna voltage supply for active
antenna.
3.3.3. VCC_IN
This is the primary 2.85V to 3.6V supply voltage for the module. A voltage of 2.85V to 3.3V
is recommended.
3.3.4. VBATT
The Battery Backup supply voltage is 2.2V to 3.3V. A typical low current supply for ensuring
the RTC/BBRAM is kept running to ensure HOT/WARM starts. Higher battery backup
supply voltages are catered for up to 3.6V.
3.3.5. Host Port
The JN3 has a single serial communications port -- UART. See the Designer’s Notes for more
details.
3.3.6. MEMS Sensor Interface
The DR I2C port is used for MEMS sensor interface. The JN3 ROM2.2 9600 baud rate
variant will not support external MEMS. Reference the Designer’s Notes for more details on
how to connect to an accelerometer and/or magnetic sensor to this port.
3.3.7. SAW Filter (1.575 GHz)
This filters the GPS signal and removes unwanted signals caused by external influences that
would corrupt the operation of the receiver. The filtered signal is fed to the RF input of
GSD4e chipset for further processing.
3.3.8. TCXO
This highly stable 16.369 MHz oscillator controls the down conversion process for the RF
block.
3.3.9. RTC
The Real Time Clock allows Hot/Warm starts and low power modes.
3.3.10. Memory
The JN3 Flash design includes a 16MB Flash storage device for operational software and
satellite data.
The JN3 EEPROM design includes a 512KB EEPROM storage device for patch code and
satellite data.
The JN3 ROM-only design does not include on-module memory. External Host memory may
be used to store patch code and satellite data.
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3.4. Physical Characteristics
The JN3 receiver has advanced miniature packaging with a base metal of copper and an
Electroless Nickel Immersion Gold (ENIG) finish.
It has 24 interface pads. These are castellated edge contacts.
3.5. Mechanical Specification
The physical dimensions of the JN3 are as follows:
- length: 16.0 mm ± 0.1 mm
- width: 12.2 mm ± 0.1 mm
- thickness: 2.4 mm ± 0.2 mm
- weight: 1 g max
Refer to Figure 2 for the JN3 mechanical layout drawing.
3.6. External Antenna Connection
The RF connection for the external antenna has a characteristic impedance of 50 ohms.
3.7. Input/Output and Power Connections
The I/O (Input / Output) and power connections use surface mount pads.
3.8. Environmental
The environmental operating conditions of the JN3 are as follows:
- temperature: 40oC to +85oC (measured on the shield)
- humidity: up to 95% non-condensing or a wet bulb temperature of +35oC
- shock (non-operating): 18 G peak, 5 ms
3.9. Compliances
The JN3 complies with the following:
- Directive 2002/95/EC on the restriction of the use of certain hazardous substances in
electrical and electronic equipment (RoHS)
- Manufactured in an ISO 9000: 2000 accredited facility
- Manufactured to TS 16949 requirement (upon request)
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3.10. Marking/Serialization
The JN3 supports a 2D barcode indicating the unit serial number below. The Telit
13-character serial number convention is:
- characters 1 and 2: year of manufacture (e.g. 12 = 2012, 13 = 2013)
- characters 3 and 4: week of manufacture (01 to 52, starting first week in January)
- character 5: manufacturer code
- characters 6 and 7: product and type
- character 8: product revision
- characters 9-13: sequential serial number
3.11. Active Antenna Gain Requirements
LNA Gain Setting
LNA Gain
(dB)
GPS Noise Figure (dB)
Recommended External
Gain Range (dB)
Low
6.0 10.0
8.5 9.5
16-30
High (default)
16.0 20.0
4.0
8-18
Table 1 Active Antenna Gain Requirements
Notes:
1. Recommended external gain range is total any external gain, such as antenna or
external LNA and any passive loss due to cables, connectors, filters, matching
network, etc.
2. In the High Gain setting an external LNA is not recommended.
3. In the Low Gain setting, the noise figure of the external LNA or active antenna must
be chosen to ensure that the total cascaded noise figure is sufficiently low to meet
overall system design requirements.
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4. Software
4.1. TTFF (Time to First Fix)
TTFF is the actual time required by a GPS receiver to achieve a valid position solution. This
specification will vary with the operating state of the receiver, the length of time since the last
position fix, the location of the last fix, and the specific receiver design.
4.1.1. Hot Start
A hot start results from a software reset after a period of continuous navigation, or a return
from a short idle period (i.e. a few minutes) that was preceded by a period of continuous
navigation. In this state, all of the critical data (position, velocity, time, and satellite
ephemeris) is valid to the specified accuracy and available in memory.
4.1.2. Warm Start
A warm start typically results from user-supplied position and time initialization data or
continuous RTC operation with an accurate last known position available in memory. In this
state, position and time data are present and valid but ephemeris data validity has expired.
4.1.3. Cold Start
A cold start acquisition results when either position or time data is unknown. Almanac
information is used to identify previously healthy satellites.
Please refer to section 5 for performance data.
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4.2. AGPS
GPS aiding comes in several forms. For the purposes of this document, we will focus on
extended ephemeris data as a form of assisted GPS data.
InstantFix (SGEE and CGEE) is a method of GPS aiding that effectively reduces the TTFF by
making every start a Hot or Warm start, through the use of ephemeris predictions.
CGEE captures ephemeris data from satellites locally and predicts ephemeris up to 3 days.
SGEE does not require local ephemeris collection from satellites; it receives the extended
ephemeris data from a server.
The module supports AGPS as standard. TELIT provides a server for customers to download
the SGEE file. Contact TELIT for support regarding this service.
Note: Due to memory size constraints, the EEPROM devices do not support SGEE.
Note: The ROM-only devices do not support CGEE or SGEE. External Host memory can be
used to enable both these features. See Designer’s Notes for more details on how to interface
with external Host memory.
4.3. Time Mark Pulse (1PPS)
A 1PPS time mark pulse is provided as an output with a width of 200ms. This signal has not
been verified or characterized for all operational conditions.
Note: The GPS receiver will only provide 1PPS when a 3D fix has been obtained using 5
SVs. When the fix degrades below a 3D solution, the 1PPS will be blanked. Once the fix
quality improves back to a 3D fix the 1PPS will again be output.
4.4. Power Management
The following paragraph describes the power management mode supported by the JN3.
4.4.1. Adaptive Trickle Power (ATP)
Trickle Power mode is a duty-cycled power management mode that reduces average current
consumption by the JN3 while retaining a high quality of GPS accuracy and dynamic motion
response. The duty cycle and navigation update rate are specified by the user to best fit in the
operating environment. This mode adapts to weak or blocked satellite signals by transitioning
the JN3 in and out of full power mode as needed in order to maintain GPS performance.
4.5. Differential Aiding
4.5.1. Satellite Based Augmentation Systems (SBAS)
The JN3 is capable of receiving WAAS, EGNOS, MSAS, and GAGAN differential
corrections which are regional implementations of SBAS. SBAS improves horizontal position
accuracy by correcting GPS signal errors caused by ionospheric disturbances, timing and
satellite orbit errors.
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4.6. 5Hz Update Rate
The JN3 defaults to an update rate of 1Hz. The JN3 can be configured to operate in 5Hz
through NMEA or SiRF Binary OSP command (v4.1.0 firmware or later). In UART mode, it
is necessary to increase the baud rate to meet the higher rate of message output from the
receiver.
For example, in NMEA, an output of RMC, GGA, and GSA at five times per second, and
GSV at once per second (GSV can be output in groups of three lines) will require at least a
baud rate of 19200. This will ensure that the messages are outputted within about 0.75
seconds.
Note that the JN3 will continue to run in 1Hz navigation until it gets a navigation fix. Once a
navigation fix is attained, it will transition into 5Hz navigation.
Utilize $PSRF103 for control in NMEA and MID136 in SiRF Binary OSP.
4.7. Dynamic Constraints
The JN3 receiver will lose track if any of the following limits are exceeded:
- ITAR limits: velocity greater than 514 m/s AND altitude above 18,288 m
- altitude: 24,000 m (max) or -500 m (min)
- velocity: 600 m/s (max)
- acceleration: 4 G (max)
- vehicle jerk: 5 m/s3 (max)
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5. Performance Data
Parameter
Description
Performance
Min
Typical
Max
Units
Horizontal
Position
Accuracy1
Autonomous
-
<2.5
-
m
Velocity
Accuracy2
Speed
-
-
<0.01
m/s
Heading
-
-
<0.01
0
Time to
First Fix3
Hot Start:
Autonomous
-
<1
-
s
Warm Start:
Autonomous
-
<35
-
s
Cold Start:
Autonomous
-
<35
-
s
Sensitivity
Autonomous
acquisition
-147
-
dBm
Tracking
-163
-
-
dBm
Navigation
-160
-
-
dBm
1. 150%, 24 hr static, -130 dBm
2. 250% @ 30 m/s
3. 350% , -130 dBm (Fu 0.5 ppm, Tu ±2 s, Pu 30 Km)
Table 2 JN3 Performance Data
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6. Electrical Requirements
6.1. Power Supply
6.1.1. VCC_IN
Main 2.85V-3.6V power input. Reference the Designer’s Notes for additional details.
Supply voltage: 2.85V to 3.6V +/- 30mV noise/ripple.
6.1.2. VBATT
Battery backup power input. 2.2V to 3.3V recommend. Maximum 3.6V supported, minimum
of 2.2V. Required for HOT/WARM starts and retention of GPS data.
6.2. External Antenna Voltage
The JN3 requires an external antenna Bias-T to provide the voltage to the antenna. This is
detailed in the Designer’s Notes.
6.3. RF (Radio Frequency) Input
RF input is 1575.42 MHz (L1 Band) at a level between 135 dBm and 165 dBm into 50
Ohm impedance.
6.4. Antenna Gain
The receiver will operate with a passive antenna with Isotropic gain down to a minimum of -
6dBi. Active antennas are supported. The internal LNA must be switched to low gain mode if
an active antenna is used.
An active antenna of 20dB minimum (exiting the cable) will offer the best performance. 30dB
exiting the antenna cable is maximum useable active antenna gain. Refer to section 2.11 for
more details.
Contact TELIT for in depth passive antenna design support.
6.5. Burnout Protection
The receiver accepts without risk of damage a signal of +10 dBm from 0 to 2 GHz carrier
frequency, except in band 1560 to 1590 MHz where the maximum level is 10 dBm.
6.6. Jamming Performance
Eight separate in band jammers can be detected and digitally removed in the GPS DSP. This
is over and above the excellent SAW filter response that exists before the GPS LNA input.
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Note: The spectral purity of oscillators and RF transmitters in the host system will determine
if harmonics are formed that are equal to the frequencies above.
Compact wireless product design requires close monitoring of jamming issues.
6.7. Flash Upgradability (Flash only)
The firmware programmed in the Flash memory may be upgraded via the serial port TX/RX
pads. The user can control this by driving the Serial BOOT select line high at startup, then
downloading the code from a PC with suitable software (SiRFFlash). In normal operation this
pad should be left floating for minimal current drain. It is recommended that in the user’s
application, the BOOT select pad is connected to a test pad for use in future software
upgrades. The JN3 Flash has a maximum flash update baud rate of 115200. Refer to the
Designer’s Notes for additional information.
6.8. Patch Updates (EEPROM only)
Modules with EEPROM can be patched from the Host using simple One Socket Protocol
(OSP) Patch Protocol serial messages. Patches are stored inside the I2C Serial EEPROM and
are automatically applied by internal firmware whenever the baseband CPU is started.
Note: ROM-only devices can support patch updates, if Host memory is available.
6.9. Data Input/Output Specifications
All communications between the JN3 receiver and external devices are through the I/O
surface mount pads. These provide the contacts for power, ground, serial I/O and control.
Power requirements are discussed in the following sections.
6.9.1. Voltages and Currents
Parameter
Symbol
Min
Typ
Max
Unit
Power Supply Voltage 1
VCC_IN
2.85
2.9 to 3.3
3.6
V
Operating Temperature 2
TOPR
-40
85
0C
Current Consumption3:
Acquisition
Tracking
41
32
mA
mA
Battery Backup Supply
VBATT
2.2
3
3.6
V
Battery Backup Current:
Flash/ ROM/EEPROM modules
40
uA
Trickle Power Current
10
mA
1. 1Ripple characteristics must be ensured for best GPS performance and reliable operation.
2. 2Operating temperature is ambient.
3. 3LNA set to High Gain Mode.
Table 3 Power Requirements
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Absolute Maximum Ratings
Parameter
Symbol
Rating
Units
Power Supply Voltage
VCC_IN
3.6
V
Input Pin Voltage
VIO_IN
3.6
V
Output Pin Voltage
VIO_OUT
3.6
V
Storage Temperature
Tstg
-40°C to +85°C
0C
Warning Stressing the device beyond the “Absolute Maximum Ratings” may cause permanent
damage. These are stress ratings only. Operation beyond the “Operating Conditions” is not
recommended and extended exposure beyond the “Operating Conditions” may affect device
reliability.
Table 4 Digital Core and I/O Voltage (Volatile)
6.9.2. DC Electrical Characteristics
6.9.2.1. TX and 1PPS
TXA and 1PPS outputs at TRISTATE until Active VCC is reached. Active VCC min is 1V.
These outputs TRISTATE if VCC reaches Ground. Maximum stress voltage on these pins is
4.5V and there is OVT protection.
VOL = 0.3V-0.4V MAX.
VOH = 0.75 x VCC typical MIN, 3.6V MAX pull up.
Typical MAX current = + 12mA, -12mA.
Normal current = +100uA to +6mA (VOL), -100uA to -6mA (VOH)
VCC = 2.85V to 3.3V typical, 3.6V MAX.
6.9.2.2. RX
VIL = 0.45V MAX.
VIH = 1.26V MIN. MAX 3.6V pull up.
Internal pull up resistance 90k ohm nominal to internal 1.8V. MAX 3.6V pull up.
INPUT/TRISTATE leakage = -10uA, +10uA.
6.9.2.3. SDA2 and SCL2
SDA2 and SCL2 outputs are in a high-impedance state until Active VCC is reached.
VOL = 0.40V MAX.
VOH = 1.35V MIN.
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6.9.2.4. BOOT (Flash only)
For normal operation, leave this pin floating. To place the JN3 into BOOT mode, tie this pin
to 1.8 volts DC.
Note: This pin is not 3.3 volt tolerant. See the Designer’s Notes for more information.
6.9.3. Pinout Description
Details of the LCC pad functions are shown in Table 5.
Pad Number
Pad Function
Type
Description
1
NC
-
No connection
2
NC
-
No connection
3
1PPS
O
Timemark Pulse, 200ms Active High
4
EXT_INT
I
Reserved
5
NC
-
No connection
6
NC
-
No connection
7
BOOT / NC
I/-
Low for run, high for reprogram (Flash only). No
connection for ROM devices.
8
NC
-
No connection
9
VCC_IN
PWR
VCC
10
GND
PWR
Ground
11
RF_IN
I
GPS RF Input, 50 Ohm
12
GND
PWR
Ground
13
GND
PWR
Ground
14
NC
-
No connection
15
NC
-
No connection
16
NC
-
No connection
17
NC
-
No connection
18
SDA2
I/O
Sensor I2C Data Port
19
SCL2
I/O
Sensor I2C Clock Port
20
TX
O
UART TX Output
21
RX
I
UART RX Input
22
VBATT
PWR
Battery Backup Voltage
23
VCC_IN
PWR
Main Supply Voltage
24
GND
PWR
Ground
Table 5 LCC Pad Functions
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7. Software Interface
The host serial I/O port of the receiver’s serial data interface supports full duplex
communication between the receiver and the user.
The default serial configuration is as follows: NMEA, 4800 bps, 8 data bits, no parity, 1 stop
bit
Note: Contact your local sales representative for details on module configurations with
default NMEA 9600 bps.
7.1. NMEA Output Messages
NMEA v3.0 is the default protocol. The following messages are output by default:
- RMC = 1 second update
- GGA = 1 second update
- GSA = 1 second update
- GSV = 5 second update (outputs at 1 second update for 9600 default variant)
Reference the NMEA protocol manual for additional message details.
7.2. SiRF OSP Output Messages
SiRF One Socket Protocol (OSP) is supported. This is an extension of the existing SiRF
Binary protocol.
The following messages are output once per second:
- MID2
- MID4
- MID9
- MID41
- MID56, 5
- MID56, 35
Reference the SiRF One Socket Protocol manual for additional message details.
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7.3. Software Functions and Capabilities
Table 6 shows the software features available to the JN3.
Feature
Description
Availability
SBAS
Improve position accuracy by using freely available satellite
based correction services called SBAS (Satellite Based
Augmentation System)
A
Adaptive Trickle Power
Improves battery life by using enhanced power management and
intelligently switching between low and full power depending
on the current GPS signal level. Refer to the Low Power
Operating Modes application note.
A
Almanac to Flash
Improves cold start times by storing the most recent almanac to
flash memory.
Yes
(Flash only)
Low Signal Acquisition
Acquires satellites and continues tracking in extremely low
signal environments.
Yes
Low Signal Navigation
Continues navigating in extremely low signal environments.
Yes
Time Mark Pulse (1PPS)
A timing pulse generated every second the receiver is in a valid
navigation state (5 SVs required for initial pulse start-up).
Yes
MEMS
3-axis accelerometer support for static detection.
3-axis magnetometer support for compass heading pass-thru
data.
A
Antenna Supervisor
Active antenna short circuit and open circuit detection/control,
software supported.
V4.1.2
SGEE
AGPS using predicted ephemeris data from a server. Supporting
Host required.
Yes
(Flash only)
CGEE
AGPS using prediction of ephemeris from live (downloaded
from satellites), ephemeris stored in memory.
Yes
(Flash/EEPROM
only)
Adaptive Jammer
Detection
System scan for up to 8 CW jammers for removal by the GPS
Yes
Yes = always enabled A = available, but not enabled by default
Table 6 Software Features
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8. Mechanical Drawing
Figure 2 Mechanical Layout
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Figure 3 Pinout (Top View)
Figure 4 3D Model
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9. Conformity Assessment
9.1. Declaration of Conformity
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9.2. R&TTE Notified Body Opinion
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10. Evaluation Kit
The JN3 Development Kit is available to assist in the evaluation and integration of the JN3
module in custom applications. The Development Kit contains all of the necessary hardware
and software to carry out a thorough evaluation of the JN3 module.
Figure 5 Evaluation Kit
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11. Product Handling
11.1. Product Packaging and Delivery
JN3 modules are shipped in Tape and Reel form. The reeled modules are shipped in 24mm
reels with 1000 units per reel. Each reel is ‘dry’ packaged and vacuum sealed in an Moisture
Barrier Bag (MBB) with two silica gel packs and placed in a carton.
The minimum order quantity for shipping is 1000 units. Refer to the Designer’s Notes for
additional details.
All packaging is ESD protective lined. The JN3 GPS receiver is a Moisture Sensitive Device
(MSD) level 3. Please follow the MSD and ESD handling instructions on the labels of the
MBB and exterior carton (refer to sections 8.2 and 8.3).
Figure 6 Tape and Reel Packaging
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11.2. Moisture Sensitivity
Precautionary measures are required in handling, storing and using such devices to avoid
damage from moisture absorption. If localized heating is required to rework or repair the
device, precautionary methods are required to avoid exposure to solder reflow temperatures
that can result in performance degradation.
Further information can be obtained from the IPC/JEDEC standard J-STD-033: Handling,
Packing, Shipping and Use of Moisture/Reflow Sensitive Surface Mount Devices.
11.3. ESD Sensitivity
The JN3 GPS receiver contains class 1 devices and is Electro-Static Discharge Sensitive
(ESDS). Telit recommends the two basic principles of protecting ESD devices from damage:
Only handle sensitive components in an ESD Protected Area (EPA) under protected and
controlled conditions
Protect sensitive devices outside the EPA using ESD protective packaging. All personnel
handling ESDS devices have the responsibility to be aware of the ESD threat to the reliability
of electronic products.
Further information can be obtained from the JESD625-A requirements for Handling
Electrostatic Discharge Sensitive (ESDS) Devices.
11.4. Safety
Improper handling and use of the Jupiter GPS receiver can cause permanent damage to the
receiver. There is also the possible risk of personal injury from mechanical trauma or choking
hazard.
11.5. Disposal
We recommend that this product should not be treated as household waste. For more detailed
information about recycling this product, please contact your local waste management
authority
or the reseller from whom you purchased the product.
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12. Ordering Information
- J-N3-B3E5-Lx JN3 Flash Module (4800 bps v4.1.2-P9)
- J-N3-B3E6-Lx JN3 Flash Module (9600 bps v4.1.2-P9)
- J-N3-B3EV-L JN3 Flash Module Evaluation Kit
- J-N3-C1E8-Fx JN3 512K EEPROM Module (4800 ROM2.2 Patch 5)
- J-N3-C1E9-Fx JN3 512K EEPROM Module (9600 ROM2.2 Patch 5)
- J-N3-C0D1-Fx JN3 ROM Module (4800 bps ROM2.2)
- J-N3-C0D2-Fx JN3 ROM Module (9600 bps ROM2.2)
NOTE: x denotes packaging type (R=Tape & Reel, Y=Tray).
Contact your local sales representative for more details.
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13. Glossary and Acronyms
AGPS: Assisted GPS. AGPS uses additional resources to locate the satellites faster and better
in poor signal conditions.
Almanac: A set of orbital parameters that allows calculation of approximate GPS satellite
positions and velocities. The almanac is used by a GPS receiver to determine satellite
visibility and as an aid during acquisition of GPS satellite signals. The almanac is a subset of
satellite ephemeris data and is updated weekly by GPS Control.
CGEE: Client Generated Extended Ephemeris data. AGPS using prediction of ephemeris
from live (downloaded from satellites), ephemeris stored in memory.
EGNOS: European Geostationary Navigation Overlay Service
The system of geostationary satellites and ground stations developed in Europe to improve the
position and time calculation performed by the GPS receiver.
Ephemeris plural ephemerides: A set of satellite orbital parameters that is used by a GPS
receiver to calculate precise GPS satellite positions and velocities. The ephemeris is used to
determine the navigation solution and is updated frequently to maintain the accuracy of GPS
receivers.
ESD: Electro-Static Discharge
large momentary unwanted currents that cause damage to electronic equipment.
GDOP: Geometric Dilution of Precision.
A factor used to describe the effect of the satellite geometry on the position and time accuracy
of the GPS receiver solution. The lower the value of the GDOP parameter, the less the error in
the position solution. Related indicators include PDOP, HDOP, TDOP and VDOP.
GPS: Global Positioning System.
A space-based radio positioning system that provides accurate position, velocity, and time
data.
InstantFix: Eliminates the initial delay of obtaining GPS satellite location data from the
satellites themselves by using algorithms to predict seven days of satellite location data.
LCC: Leadless Chip Carrier
A surface mount device that uses surfaces on the side of its body for board attachment and has
no leads or legs but has rounded pins through the edges of the ceramic or molded plastic
package.
MSD: Moisture sensitive device.
NMEA: National Marine Electronics Association
POR: Power on Reset.
SBAS: Satellite Based Augmentation System
Any system that uses a network of geostationary satellites and ground stations to improve the
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performance of a Global Navigation Satellite System (GNSS). Current examples are EGNOS
and WAAS.
SGEE: Server Generated Extended Ephemeris data. AGPS using predicted ephemeris data
from a server. Supporting Host required.
WAAS: Wide Area Augmentation System
The system of satellites and ground stations developed by the FAA (Federal Aviation
Administration) that provides GPS signal corrections. WAAS satellite coverage is currently
only available in North America.
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14. Safety Recommendations
READ CAREFULLY
Be sure the use of this product is allowed in the country and in the environment required. The
use of this product may be dangerous and has to be avoided in the following areas:
Where it can interfere with other electronic devices in environments such as hospitals,
airports, aircrafts, etc.
Where there is risk of explosion such as gasoline stations, oil refineries, etc. It is
responsibility of the user to enforce the country regulation and the specific
environment regulation.
Do not disassemble the product; any mark of tampering will compromise the warranty
validity. We recommend following the instructions of the hardware user guides for a correct
wiring of the product. The product has to be supplied with a stabilized voltage source and the
wiring has to be conforming to the security and fire prevention regulations. The product has to
be handled with care, avoiding any contact with the pins because electrostatic discharges may
damage the product itself.
The system integrator is responsible of the functioning of the final product; therefore, care has
to be taken to the external components of the module, as well as of any project or installation
issue. Should there be any doubt, please refer to the technical documentation and the
regulations in force. Every module has to be equipped with a proper antenna with specific
characteristics. The antenna has to be installed with care in order to avoid any interference
with other electronic devices.
The European Community provides some Directives for the electronic equipments
introduced on the market. All the relevant information’s are available on the European
Community website:
http://ec.europa.eu/enterprise/sectors/rtte/documents/
The text of the Directive 99/05 regarding telecommunication equipments is available,
while the applicable Directives (Low Voltage and EMC) are available at:
http://ec.europa.eu/enterprise/sectors/electrical/
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15. Document History
Revision
Date
Changes
0
2012-01-19
First issue
1
2012-04-23
§5.9.2.3 updated I2C voltage range
Updated figure 3
2
2012-12-17
Updated ordering information,
Updated table 3 of §5.9.1 about ROM/EEPROM hibernate
current consumption
Inserted § 8 Conformity Assessment
3
2013-04-19
Update section 3
Add section 4.6 for 5Hz
Update formatting
Update Ordering information
4
2013-05-15
Update section 8 added pin 1 designations and clarified
bottom side and top references.
5
2015-07-09
Updated §12 ordering information
Update §14 safety recommendations