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GPS定位系统/车载终端/GPS测试软件模组BU-1315

 
品牌: 百年星
单价: 1.00元/片
起订: 1 片
供货总量: 1000000 片
发货期限: 自买家付款之日起 3 天内发货
所在地: 广东 深圳
有效期至: 长期有效
最后更新: 2015-07-10 18:12
浏览次数: 78
 
公司基本资料信息
详细说明
 1 .Introduction 
The BNSTAR BU-1315 module is a high sensitivity, low power and very compact Surface Mount 
Device (SMD), and it supports signal processing of L1 band signals such as GPS C/A and SBAS 
(including WAAS, EGNOS, and MSAS). This 56-channel global positioning system (GPS) 
receiver is designed for a broad spectrum of OEM applications and is based on the fast and 
deep GPS signal search capabilities. BNSTAR BU-1315 is designed to allow quick 
and easy integration into GPS-related applications, especially for compact size devices, such 
as: 
 PDA, Pocket PC and other computing devices 
 Fleet Management / Asset Tracking 
 AVL and Location-based Services 
 Hand-held Device for Personal Positioning and Navigation 
1.1 Features 
Hardware and Software 
 56 acquisition channels and achieve -162dBm tracking 
 Compact module size for easy integration: 15x13x2.5 mm. 
 SMT pads allow for fully automatic assembly processes equipment and reflow soldering 
 Built-in LDO, regulators to decrease extra-BOM cost 
 Up to 10Hz updat rate 
 Embedded DC/DC circuitry to prolong battery life 
 AGPS supported 
 
Performance 
 Cold/Warm/Hot Start Time: 29 / 28 / 1 sec. 
 RF metal Shield for best performance in noisy environments 
 Enhanced Navigation Performance 
 
Interface 
 TTL level UART interface 
 Protocol: NMEA 
 Baud Rate: 9600 bps(Default) 
 
Advantages 
 Ideal for compact size devices 
 Data / Power / RF through surface mount pads 
 Flexible and cost effective hardware design for different application requirements 
 Secure SMD PCB mounting method  
2. Pin Assignment 
 
 
Pin Numbers Name Type Description Note 
1,2,6,7,8,9,10,
13,14,15 
 NC NC 
3 1PPS O One pulse per second output 
4 UART TXD O TTL UART output,0~3.3V 
5 UART RXD I TTL UART input 
9 GPO O general purpose output. NC if not 
used 
 
11 VBAT P Backup battery supply voltage 
12 VCC_MAIN P Main power supply voltage 
16 SAFEBOOT_N I Safe boot input. Low asserted. 
Note: DO NOT tie to GND in 
 normal mode 
17 VCC_RF P Supply Antenna Bias voltage(V = 
Vcc) 
 
19 RF_IN I GPS Antenna Input 
18,20,21,22, GND P Ground 
3. Electrical Specification 
3.1 Absolute maximum ratings 
 
Parameter Symbol Min Max Unit 
Power Supply Voltage VCC_MAIN -0.5 3.6 V 
Backup Supply Voltage VBAT -0.5 3.6 V 
 
3.2 Operation Conditions 
 
Parameter Symbol Min Typ Max Unit 
Main Power Supply 
Power Supply Voltage VCC_MAIN 1.8 3.3 3.6 V 
Operating Current 26 mA 
Backup Power Supply 
Backup Supply Voltage VBAT 1.6 3.3 3.6 V 
Operating Current(Working) 185 uA 
Operating Current(Sleep) 15 uA 
UART and IO 
Input Low Voltage Vil 0 0.72 V 
Input High Voltage Vih 2.0 3.6 V 
Output Low Voltage Vol 0.4 V 
Output High Voltage Voh 2.4 V 
 
 
 
 
 
 
 
 
 
  3.3 Environmental Specification 
 
Item Description 
Operating temperature range -40 deg. C to +85 deg. C 
Storage temperature range -40 deg. C to +85 deg. C 
Altitude 50,000 m 
Velocity 500 m/s 
Jerk 
 
4. Reference Design 
 
 
 
Note: 
1.Trace impedance between Antenna and Pin19 should be 50 ohm. 
2.Trace between Antenna and L1 inductor is recommended to be 5mil line width. 
3.For L1 inductor selecion, Impedance > 500 ohm @GPS frequency is better. 
 
 
 
 
M1
NC
1
NC
2
1PPS
3
UART_TX
4
UART_RX
5
GND
21
NC
6
NC
7
NC
8
GPIO/ANT_OFF
9
NC
10
VBAT
11
VCC_MAIN
12
NC
13
NC
14
NC
15
GND
22
SAFEBOOT_N
16
VCC_RF
17
GND
18
RF_IN
19
GND
20
E1
GPS_ANT
L1
33nH
C3
1uF
C2
1nF
VCC_Main_Power
D1
R1 BT1
0 ohm
C4
1uF
C5
1uF
UART TX
1PPS
UART RX5. Performance Characteristics 
Position and Velocity Accuracy 
Accuracy Position 2.5m in autonomous 
2.0m in SBAS 
Velocity 0.1 m/s 
 
 
Dynamic constrains 
Dynamic Conditions Altitude 50,000m 
Velocity 500 m/s 
Acceleration <= 4g 
 
Acquisition time TTFF 
Item Description 
Hot Start 1s 
Warm Start 28s 
Cold Start 29s 
 
Sensitivity 
Parameter Description 
Tracking & Navigation -162 dBm 
Acquisition -148 dBm 
 
 
 
 
 
 6. PCB Layout Recommend 
Recommended Layout Pad 
 
PCB Layout Recommendations 
 Do not routing the other signal or power trace under the module board. 
RF: 
 This pin receives signal of GPS analog via external active antenna. Note: It has to be a 
controlled impedance trace at 50ohm. 
 Do not place the RF traces close to the other signal path and not routing it on the top layer. 
 Keep the RF traces as short as possible. 
Antenna: 
 Keep the active antenna on the top of your system and confirm the antenna radiation pattern、 
axial ratio、power gain、noise figure、VSWR are correct when you Setup the antenna in your case. 
 
 7. Configuration Management 
Configuration settings can be modified with configuration messages. The modified settings remain 
effective until power-down or reset. If these settings have been stored in battery-backup RAM, 
then the modified configuration will be retained, as long as the backup battery supply is not 
interrupted. 
Note that: If any new configuration needs to be done, pls refer to module Receiver Description 
Including Protocol Specification. 
 
8 Software Interface 
The output NMEA (0183 v3.01) messages for the receiver are listed as below. 
NMEA Command Description 
GGA Time, position, and fix related data for a GPS receiver. 
GLL Latitude and longitude of present position, time of position fix and 
status 
GSA GPS receiver operating mode, satellites used in the position 
solution, and DOP values. 
GSV The number of GPS satellites in view satellite ID numbers, 
elevation, azimuth, and SNR values. 
RMC Time, date, position, course and speed data provided by the GPS 
receiver. 
 
GGA - Global Positioning System Fixed Data 
For example: 
$GPGGA,161229.487,3723.24751,N,12158.34162,W,1,07,1.0,9.0,M,-34.2,M,,0000*18 
Table 1 
Name Example Description Unit 
Message ID $GPGGA GGA protocol header 
UTC Time 161229.487 hhmmss.sss 
Latitude 3723.24751 ddmm.mmmmm 
N/S Indicator N N=north or S=south 
Longitude 12158.34162 dddmm.mmmmm 
E/W Indicator W E=east or W=west 
Position Fix Indicator 1 See Table 1-1 
Satellites Used 07 Range 0 to 12 
HDOP 1.0 Horizontal Dilution of Precision MSL Altitude 9.0 meters 
Units M meters 
Geoid Separation -34.2 Geoid-to-ellipsoid separation. 
Ellipsoid altitude=MSL Altitude + Geoid 
Separation 
meters 
Units M meters 
Age of Diff. Corr. Null fields when DGPS is not used second 
Diff. Ref. Station ID 0000 
Checksum *18 
<CR><LF> End of message termination 
 
Table 1-1 
Value Description 
0 Fix not available or invalid 
1 GPS SPS Mode, fix valid 
2 Differential GPS, SPS Mode , fix valid 
3 Not supported 
6 Dead Reckoning Mode, fix valid 
 
GLL - Geographic Position-Latitude/Longitude 
For example: 
$GPGLL,3723.24755,N,12158.34166,W,161229.487,A,A*41 
Table2 
Name Example Description Unit 
Message ID $GPGLL GLL protocol header 
Latitude 3723.24755 ddmm.mmmmm 
N/S Indicator N N=north or S=south 
Longitude 12158.34166 dddmm.mmmmm 
E/W Indicator W E=east or W=west 
UTC Position 161229.487 hhmmss.sss 
Status A A=data valid or V=data not valid 
Mode A A=Autonomous, D=DGPS, 
E=DR 
N=Output Data Not Valid 
R= Coarse Position1 
S=Simulator 
 Checksum *41 
<CR><LF> End of message termination 
1.Position was calculated based on one or more of the SVs having their states derived from 
almanac parameters, as opposed to ephemerides. 
 
GSA - GNSS DOP and Active Satellites 
For example: 
$GPGSA,A,3,07,02,26,27,09,04,15,,,,,,1.8,1.0,1.5*33 
Table3 
Name Example Description Unit 
Message ID $GPGSA GSA protocol header 
Mode 1 A See Table 3-1 
Mode 2 3 See Table 3-2 
Satellite Used1 07 Sv on Channel 1 
Satellite Used1
 02 Sv on Channel 2 
…… 
Satellite Used1
 Sv on Channel 12 
PDOP2 1.8 Position dilution of Precision 
HDOP2 1.0 Horizontal dilution of Precision 
VDOP2 1.5 Vertical dilution of Precision 
Checksum *33 
<CR><LF> End of message termination 
1. Satellite used in solution. 
2. Maximum DOP value reported is50. When 50 is reported, the actual DOP may be much 
larger. 
Table3-1 
Value Description 
M Manual-forced to operate in 2D or 3D 
mode 
A Automatically switch in 2D or 3D mode 
 
Table3-2 
Value Description 
1 Fix Not Available 
2 2D (<4 SVs used) 
3 3D (>3 SVs used)  
 
GSV - GNSS Satellites in View 
For example: 
$GPGSV,2,1,07,07,79,048,42,02,51,062,43,26,36,256,42,27,27,138,42*71 
$GPGSV,2,2,07,09,23,313,42,04,19,159,41,15,12,041,42*41 
Table4 
Name Example Description Unit 
Message ID $GPGSV GSV protocol header 
Number of Messages1 2 Range 1 to 3 
Message Number1 1 Range 1 to 3 
Satellites in View1 07 
Satellite ID 07 Channel 1(Range 1 to 32) 
Elevation 79 Channel 1(Maximum90) degrees 
Azimuth 048 Channel1(True, Range 0 to 359) degrees 
SNR(C/No) 42 Range 0 to 99,null when not tracking dBHz 
…… …… 
Satellite ID 27 Channel 4 (Range 1 to 32) 
Elevation 27 Channel 4(Maximum90) degrees 
Azimuth 138 Channel4(True, Range 0 to 359) degrees 
SNR(C/No) 42 Range 0 to 99,null when not tracking dBHz 
Checksum *71 
<CR><LF> End of message termination 
1. Depending on the number of satellites tracked, multiple messages of GSV data may be 
required. In some software versions, the maximum number of satellites reported as visible is 
limited to 12, even though more may be visible. 
 
RMC - Recommended Minimum Specific GNSS Data 
For example: 
$GPRMC,161229.487,A,3723.24755,N,12158.34166,W,0.13,309.62,120598,,,A*10 
Table5 
Name Example Description Unit 
Message ID $GPRMC RMC protocol header 
UTC Time 161229.487 hhmmss.sss 
Status1 A A=data valid or V=data not valid Latitude 3723.24755 ddmm.mmmmm 
N/S Indicator N N=north or S=south 
Longitude 12158.34166 dddmm.mmmmm 
E/W Indicator W E=east or W=west 
Speed Over Ground 0.13 knots 
Course Over Ground 309.62 True degrees 
Date 120598 ddmmyy 
Magnetic Variation2 E=east or W=west degrees 
East/West Indicator2 E E=east 
Mode A A=Autonomous, D=DGPS, 
E=DR 
N=Output Data Not Valid 
R= Coarse Position3 
S=Simulator 
 
Checksum *10 
<CR><LF> End of message termination 
1. A valid status is derived from all the parameters set in the software. This includes the minimum 
number of satellites required, any DOP mask setting, presence of DGPS corrections, etc. If the 
default or current software setting requires that a factoris met, then if that factor is not met the 
solution will be marked as invalid. 
2. All “course over ground” data are geodetic WGS84 directions relative to true North. 
3. Position was calculated based on one or more of the SVs having their states derived from 
almanac parameters, as opposed to ephemerides. 
 
 
 
 
 
 
 
 
  
9 .Recommended Reflow Profile 
High quality, low defect soldering requires identifying the optimum temperatur
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