RFSOLUTIONS GPS-622F

GPS SMART RECEIVER WITH ANTENNA
GPS-622F
LowLow-Power HighHigh-Performance and LowLow-Cost
65 Channel GPS Engine Board (Flash based)
Data Sheet
Abstract
Technical data sheet describing the cost effective, high-performance
GPS622F
GPS622F based series of ultra high sensitive GPS modules.
The GPS622F
GPS622F is a GPS module that is sensitive to
electrostatic dis(ESD). Please handle with appropriate care.
dis- charge (ESD)
The Acceptability of Electronic Assemblies of this module
has been under IPCIPC-A-610D specification
DS-GPS-622F-2
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
Version History
Rev.
Date
1.0
12-07-09
2.0
01-03-10
Description
Description
Initial Draft – preliminary information
Adding the Internal Antenna Specification
Flash Version Support the following Features
Binary cod e
Selectab le NMEA Outp ut Data Sentences
Selectab le Serial Port Settings. (4800/9600/38400/115200b p s.
Default : 9600)
DS-GPS-622F-2
Selectab le up d ate rate (1 / 2 / 4 / 5 / 8 / 10 H z up d ate rate (1H z d efault))
Firmw are Up grad eab le
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
1 Functional Description
1.1 Introduction
The GPS-622F a highly integrated smart GPS module with a ceramic GPS patch antenna. The
antenna is connected to the module via an LNA. The module is with 54 channel acquisition engine
and 14 channel track engine, which be capable of receiving signals from up to 68 GPS satellites and
transferring them into the precise position and timing information that can be read over UART port.
Small size and high-end GPS functionality are at low power consumption, the LVTTL-level signal
interface is provided on the interface connector, supply voltage of 3V~5.5V is supported.
The compact 22mm x 22mm form factor allows it to be used in many applications.
The smart GPS antenna module is available as an off-the-shelf component, 100% tested. The smart
GPS antenna module can be offered for OEM applications with the versatile adaptation in form and
connection. Additionally, the antenna can be tuned to the final systems’ circumstances.
1.2 Features
68 C hannel GPS L 1 C /A C od e
Perform 8 million time-freq uency hyp othesis testing p er second
65 C hannel GPS L 1 C /A C od e
Perform 8 million time-freq uency hyp othesis testing p er second
Op en sky hot start 1 sec, Op en sky cold start 29 sec
Signal d etection b etter than -165d Bm
Multip ath d etection and sup p ression
Accuracy 2.5m C EP
Maximum up d ate rate 20H z
Tracking current ~33Ma
Sup p orts external active antenna
1.3 Applications
DS-GPS-622F-2
Automotive and Marine Navigation
Automotive Navigator Tracking
Emergency Locator
Personal Positioning
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
2 Characteristics
2.1 General Specification
Paramet
Parameter
Specification
68 Channels
Rec
Receiver Type
TimeTime-ToTo-First-Fix
Fix
Sensitivi
Sensitivity
Accuracy
Update Rate
Veloci
Velocity Accuracy
Accuracy
Headi
eading Accuracy
Accuracy
Dynamics
Operati
ational Limits
GPS L1 frequency, C/A Code
Cold Start (Autonomous)
29s (Average, under open sky)
Warm Start (Autonomous)
29s (Average, under open sky)
Hot Start (Autonomous)
29s (Average, under open sky)
Tracking & Navigation
-165 dBm
Reacquisition
-158 dBm
Cold Start (Autonomous)
-148 dBm
Autonomous
2.5 m CEP
Velocity
0.1 m/sec (without aid)
Time
300 ns
Supports 1 / 2 / 4 / 5 / 8 / 10 Hz update Rate (1Hz default)
0.1m/s
0.5 degrees
4 G (39.2 m/sec)
515 m/s (1000 knots)
Velocity
Altitude
<18000 meters
(COCOM limit, either may be exceeded but not both)
Serial Interface
LVTTL level
Datum
Default WGS-84
User definable
Input Voltage User
Input Current
3.3V -5.5V DC +/-10%
~23 mA tracking
Dimension
22L x 22W x H (mm)
Weight
25g
Chipset
Venus 6
Table 1: GPSGPS-622F general specification
specification
*: GPGGA, GPGSA, GPGSV, GPRMC, GPVTG are default output message
DS-GPS-622F-2
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
2.2 Serial Port Settin
Settings
The default configuration within the standard GPS firmware is the Standard configuration of
serial port:
Supporting 9600 baud rate, 8 data bits, no parity, 1 stop bit, no flow control
2.3
2.3 GPS Status Indicator
NonNon-Fixed mode : LED is always on
Fixed mode : LED toggle every second
1. Communication Specifications
Item
Description
Interface
Full duplex serial interface
Bit rate
Default 9600
Start bit
1bit
Stop bit
1bit
Data bit
8bit
Parity
None
Transmission data
SACII NMEA0183 Ver:3.01
Update rate
1Hz
Output sentence
GGA/GSA/GSV/RMC/VTG (typ)
Table 2: Communication specifications
2.6 MultiMulti-path Mitigation
Multipath refers to the existence of signals reflected from objects in the vicinity of a receiver's
antenna that corrupt the direct line-of-sight signals from the GPS satellites, thus degrading
the accuracy of both code-based and carrier phase–based measurements. Particularly difficult
is close-in multipath in which the reflected secondary signals arrive only slightly later (within
about 100 nanoseconds) than does the direct-path signal, having been reflected from objects
only a short distance from the receiver antenna.
GPS-622F deploys the advanced multi-path detection and suppression algorithm to reduce
multipath errors, the GPS signals themselves can be designed to provide inherent resistance
to multipath errors
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
2.7 Operating Conditions
Description
Vcc
Min
2.7v
Typical
3.3v
Max
5.5v
Enhanced-mode Acquisition
70 mA
Low power Acquisition Current
50mA
Tracking Current
23mA
Table 3: Operating Conditions
2.8 1PPS
PPS Output
put
The GPS receiver is in navigation mode upon power-up, with 1PPS output free running. After 3
minutes of valid position fix and remaining under static-mode, the receiver changes to timingmode, with 1PPS output signal synchronized to the UTC second. The receiver will change to
navigation-mode, with 1PPS output free running, if the receiver is in motion. The 1PPS output
will become synchronized to the UTC second again after the receiver had remained in static
mode for 3 minutes.
2.9 Antenna
A numbers of important properties of GNSS antennas affect functionality and performance,
including;
Frequency coverage
Gain pattern
Circular polarization
Multipath suppression
Phase Centre
Impact on receiver sensitivity
Interference handling
The GPS-622F module is designed to work both active and passive antenna. Active antenna
with gain in range of 10 ~ 30dB and noise figure less than 2dB can be used.
2.10 Mechanical Characteristics
Mechanical dimensions
Length
Width
Height
Weight
DS-GPS-622F-2
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22 mm
22 mm
8 mm
30g (may vary)
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
3 PINOUT DESCRIPTION
Pin Number
Signal Name
Description
1
RXD
UART input, 3V LVTTL for SUP500R, SUP500RB
2
TXD
UART output, 3V LVTTL for SUP500R, SUP500RB
UART output, RS232 level for SUP500RR
3
GND
GND
System ground
4
VDD
Main3.3V ~ 5.5V supply input
5
VBAT*
VBAT*
Backup supply voltage for RTC and SRAM, 1.5V ~ 5.5V
6
P1PS
1 pulse per second time mark output
7
PSE_SEL
Search Engine Mode select:
1: Low power acquisition mode (default), acquisition current
~50mA
0: Enhanced acquisition mode, acquisition current ~70mA
* Note: Both VDD and VBAT need to be connected in order for the module to work.*
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
4. Mechanical
Mechanical Characteristics
DS-GPS-622F-2
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
Table 4: Pin definition
4. Environmental Conditions
Parameter
Specification
Temperature Storage
℃
℃
-40℃~+85
~+85℃
Humidity
5%~95%
Storage
6 months in original vacuum package.
Operating
-40 ~+85
~+85
Table 5: Environmental
Environmental conditio
conditions
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
5. NMEA protocol
The serial interface protocol is based on the National Marine Electronics Association’s NMEA
0183 ASCII interface specification. This standard is fully define in “NMEA 0183, Version 3.01”
The standard may be obtained from NMEA, www.nmea.org
5.1 GGAGGA-GLOBAL POSITIONING SYSTEM FIX DATA
Time, position and fix related data for a GPS receiver.
Structure:
$GPGGA,hhmmss.sss,ddmm.mmmm,a,dddmm.mmmm,a,x,xx,x.x,x.x,M,x.x,M,x.x,xxxx*hh<CR><LF>
1
2
3
4
5
6 7 8 9
10
11 12 13
Example:
$GPGGA,060932.448,2447.0959,N,12100.5204,E,1,08,1.1,108.7,M,,,,0000*0E<CR><LF>
Field Name
Example
1
UTC Time
060932.448
2
Latitude
2447.0959
Description
UTC of position in hhmmss.sss format, (000000.00 ~
235959.99)
Latitude in ddmm.mmmm format
Leading zeros transmitted
3
N/S Indicator N
4
Longitude
Latitude hemisphere indicator, ‘N’ = North, ‘S’ = South
Longitude in dddmm.mmmm format
12100.5204
Leading zeros transmitted
5
E/W Indicator E
Longitude hemisphere indicator, 'E' = East, 'W' = West
GPS quality indicator
0: position fix unavailable
1: valid position fix, SPS mode
GPS quality
6
indicator
2: valid position fix, differential GPS mode
1
3: GPS PPS Mode, fix valid
4: Real Time Kinematic. System used in RTK mode with fixed
integers
5: Float RTK. Satellite system used in RTK mode. Floating
integers
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
6: Estimated (dead reckoning) Mode
7: Manual Input Mode
8: Simulator Mode
7
Satellites
Used
08
Number of satellites in use, (00 ~ 12)
8
HDOP
1.1
Horizontal dilution of precision, (00.0 ~ 99.9)
9
Altitude
108.7
mean sea level (geoid), (-9999.9 ~ 17999.9)
10
Geoid
Geoid separation in meters according to WGS-84 ellipsoid (-
Separation
999.9 ~ 9999.9)
Age of DGPS data since last valid RTCM transmission in xxx
format (seconds)
11 DGPS Age
NULL when DGPS not used
12
DGPS Station
ID
13 Checksum
Differential reference station ID, 0000 ~ 1023
0000
NULL when DGPS not used
0E
Note: The checksum field starts with a ‘*’ and consists of 2 characters representing a hex
number. The checksum is the exclusive OR of all characters between ‘$’ and ‘*’.
DS-GPS-622F-2
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GPS-622F
5.2 GLL - LATITUDE AND LONGITUDE, WITH TIME OF POSITION FIX AND STATUS
Latitude and longitude of current position, time, and status.
Structure:
$GPGLL,ddmm.mmmm,a,dddmm.mmmm,a,hhmmss.sss,A,a*hh<CR><LF>
1
2
3
4
5
6
7
8
Example:
$GPGLL,4250.5589,S,14718.5084,E,092204.999,A,A*2D<CR><LF>
Field Name
Example
Description
Latitude in ddmm.mmmm format
1
Latitude
4250.5589
Leading zeros transmitted
Latitude hemisphere indicator
2
N/S Indicator
S
‘N’ = North
‘S’ = South
Longitude in dddmm.mmmm format
3
Longitude
14718.5084
Leading zeros transmitted
Longitude hemisphere indicator
4
E/W Indicator
E
'E' = East
'W' = West
5
UTC Time
092204.999
6
Status
A
UTC time in hhmmss.sss format (000000.00 ~
235959.99)
Status, ‘A’ = Data valid, ‘V’ = Data not valid
Mode indicator
‘N’ = Data not valid
‘A’ = Autonomous mode
7
Mode Indicator
A
‘D’ = Differential mode
‘E’ = Estimated (dead reckoning) mode
‘M’ = Manual input mode
‘S’ = Simulator mode
8
DS-GPS-622F-2
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Checksum
2D
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
5.3 GSA - GPS DOP AND ACTIVE SATELLITES
GPS receiver operating mode, satellites used in the navigation solution reported by the GGA or
GNS sentence and DOP values.
Structure:
$GPGSA,A,x,xx,xx,xx,xx,xx,xx,xx,xx,xx,xx,xx,xx,x.x,x.x,x.x*hh<CR><LF>
123 3 3 3 3 3 3 3 3 3 3 3 4 5 6
7
Example:
$GPGSA,A,3,01,20,19,13,,,,,,,,,40.4,24.4,32.2*0A<CR><LF>
Field Name
Example
Description
Mode
1
Mode
A
‘M’ = Manual, forced to operate in 2D or 3D mode
‘A’ = Automatic, allowed to automatically switch
2D/3D
Fix type
1 = Fix not available
2
Mode
3
2 = 2D
3 = 3D
3
DS-GPS-622F-2
Satellite
used 01,20,19,13, Satellite ID number, 01 to 32, of satellite used in
1~12
,,,,,,,,
solution, up to 12 transmitted
4
PDOP
40.4
Position dilution of precision (00.0 to 99.9)
5
HDOP
24.4
Horizontal dilution of precision (00.0 to 99.9)
6
VDOP
32.2
Vertical dilution of precision (00.0 to 99.9)
7
Checksum
0A
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
5.4 GSV - GPS SATELLITE IN VIEW
Numbers of satellites in view, PRN number, elevation angle, azimuth angle, and C/No. Four
satellites details are transmitted per message. Additional satellite in view information is send
in subsequent GSV messages.
Structure:
$GPGSV,x,x,xx,xx,xx,xxx,xx,…,xx,xx,xxx,xx *hh<CR><LF>
123 4 5 6 7
4 5 6 7 8
Example:
$GPGSV,3,1,09,28,81,225,41,24,66,323,44,20,48,066,43,17,45,336,41*78<CR><LF>
$GPGSV,3,2,09,07,36,321,45,04,36,257,39,11,20,050,41,08,18,208,43*77<CR><LF>
Field NaME
1
Number of
message
Example
Description
3
Total number of GSV messages to be transmitted (1-3)
2
Sequence number 1
Sequence number of current GSV message
3
Satellites in view
09
Total number of satellites in view (00 ~ 12)
4
Satellite ID
28
5
Elevation
81
Satellite elevation in degrees, (00 ~ 90)
6
Azimuth
225
Satellite azimuth angle in degrees, (000 ~ 359 )
7
SNR
41
Satellite ID number, GPS: 01 ~ 32, SBAS: 33 ~ 64 (33
= PRN120)
C/No in dB (00 ~ 99)
Null when not tracking
8
DS-GPS-622F-2
Checksum
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
5.5 RMC - RECOMMANDED MINIMUM SPECIFIC GPS/TRANSIT DATA
Time, date, position, course and speed data provided by a GNSS navigation receiver.
Structure:
$GPRMC,hhmmss.sss,A,dddmm.mmmm,a,dddmm.mmmm,a,x.x,x.x,ddmmyy,x.x,a,a*hh<CR><LF>
1
2
3
4
5
6 7
8
9 10 11 12
13
Example:
$GPRMC,092204.999,A,4250.5589,S,14718.5084,E,0.00,89.68,211200,,A*25<CR><LF>
Field NaME
1
2
3
4
5
6
7
8
9
10
11
12
13
DS-GPS-622F-2
Description
UTC time in hhmmss.sss format (000000.00 ~
UTC time
092204.999
235959.999)
Status
Status
A
‘V’ = Navigation receiver warning
‘A’ = Data Valid
Latitude in dddmm.mmmm format
Latitude
4250.5589
Leading zeros transmitted
Latitude hemisphere indicator
N/S indicator
S
‘N’ = North
‘S’ = South
Longitude in dddmm.mmmm format
Longitude
14718.5084
Leading zeros transmitted
Longitude hemisphere indicator
E/W Indicator
E
'E' = East
'W' = West
Speed over ground 000.0
Speed over ground in knots (000.0 ~ 999.9)
Course
over
000.0
Course over ground in degrees (000.0 ~ 359.9)
ground
UTC Date
211200
UTC date of position fix, ddmmyy format
Magnetic variation
Magnetic variation in degrees (000.0 ~ 180.0)
Magnetic variation direction
Magnetic Variation
‘E’ = East
‘W’ = West
Mode indicator
‘N’ = Data not valid
‘A’ = Autonomous mode
Mode indicator
A
‘D’ = Differential mode
‘E’ = Estimated (dead reckoning) mode
‘M’ = Manual input mode
‘S’ = Simulator mode
checksum
25
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Example
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
5.6 VTG - COURSE OVER GROUND AND GROUND SPEED
The Actual course and speed relative to the ground.
Structure:
GPVTG,x.x,T,x.x,M,x.x,N,x.x,K,a*hh<CR><LF>
1
2
3
4
5 6
Example:
$GPVTG,89.68,T,,M,0.00,N,0.0,K,A*5F<CR><LF>
Field Name
1
Course
Example
89.68
2
Course
3
Speed
0.00
4
Speed
0.00
5
Mode
A
6
Checksum
5F
Description
True course over ground in degrees (000.0 ~ 359.9)
Magnetic course over ground in degrees (000.0 ~
359.9)
Speed over ground in knots (000.0 ~ 999.9)
Speed over ground in kilometers per hour (0000.0 ~
1800.0)
Mode indicator
‘N’ = not valid
‘A’ = Autonomous mode
‘D’ = Differential mode
‘E’ = Estimated (dead reckoning) mode
‘M’ = Manual input mode
‘S’ = Simulator mode
5.7 ZDAZDA- TIME AND DATE
Structure:
$GPRMC,hhmmss.sss,dd,mm.yyyy, , ,xxx<CR><LF>
1
2 3 4 5
6
7
Example:
$GPZDA,104548.04,25,03,2004,,*6C<CR><LF>
Field
Name
Example
1
UTC time
2
UTC time: day 25
UTC
time:
03
month
UTC time: year 2004
3
4
104548.04
5
6
7
DS-GPS-622F-2
Sept 11
6C
6C
Description
UTC time in hhmmss.ss format, 000000.00 ~
235959.99
UTC time day (01 ... 31)
UTC time: month (01 ... 12)
UTC time: year (4 digit year)
Local zone hour
Not being output by the receiver (NULL)
Local zone minutes
Not being output by the receiver (NULL)
Checksum
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GPS SMART RECEIVER WITH ANTENNA
GPS-622F
6. Links
http://www.skytraq.com.tw/download/AN0003_v3.pdf - Skytraq Application Note AN0003
http://www.sparkfun.com/datasheets/GPS/Modules/AN0003_v1.4.8.pdf
Please note that not all the commands in the application note apply for this module; for additional information please contact
SkyTraq directly.
7. Contact Information
We hope this datasheet will be helpful to the user to get the most out of the GPS
module, furthermore feedback inputs about errors or mistakable verbalizations and
comments or proposals to RF Solutions Ltd.
Ltd.. for further improvements are highly
appreciated.
© 2011
2011 RF Solutions Ltd.
Ltd. All right
rights reser
reserved.
Not to be reproduced in whole or part for any purpose without written permission of RF
Solutions Ltd.
Ltd Information provided by RF Solutions Ltd is believed to be accurate and reliable.
These materials are provided by RF Solutions Ltd as a service to its customers and may be
used for informational purposes only. RF Solutions Ltd assumes no responsibility for errors or
omissions in these materials, nor for its use RF Solutions
Solutions Ltd reserves the right to change
specification at any time without notice.
These materials are provides “as is” without warranty of any kind, either expressed or implied,
relating to sale and/or use of RF Solutions Ltd products including liability or warranties
relating
to
fitness
for
a
particular
purpose,
consequential
or
incidental
damages,
merchantability, or infringement of any patent, copyright or other intellectual property right.
RF Solutions Ltd further does not warrant the accuracy or completeness of the information,
text, graphics or other items contained within these materials. RF Solutions Ltd shall not be
liable for any special, indirect, incidental, or consequential damages, including without
limitation, lost revenues or lost profits, which may result from the use of these materials.
RF Solutions Ltd products are not intended for use in medical, life-support devices, or
applications involving potential risk of death, personal injury, or severe property damage in
case of failure of the product.
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