AllyNav R51 GNSS Receiver User Manual
- June 8, 2024
- AllyNav
Table of Contents
AllyNav R51 GNSS Receiver
revision history
revision number | Revision Notes | Revised by | date |
---|---|---|---|
V 1.0 | Publish first draft | Zhang Bing | April 2021 _ |
V 1.1 | Supplementary solar controller and gyroscope description section | Zhang | |
Bing | April 2021 _ |
forward Word
Introduction
Welcome to the R51 Universal Receiver Product Instruction Manual. This manual mainly takes the R51 receiver as an example to describe how to install, set up and use this series of products.
Disclaimer
Liangshan Navigation Co., Ltd. is committed to continuous improvement of
product functions and performance. Later product specifications and manual
contents may be changed accordingly without prior notice, please understand!
If the icons, pictures, etc. in the manual are different from the actual
product, please refer to the actual product. The company reserves the right of
final interpretation of all technical parameters and graphic information.
Before using this product, please read this instruction manual carefully. For
the loss caused by disoperation of this product without following the
requirements of the instruction manual or failing to correctly understand the
requirements of the instruction manual, Liangshan will not be responsible for
any loss.
This product is designed to withstand certain harsh environments. However,
this device is a high precision electronic instrument and should be treated
with care. Operating or storing the receiver outside the specified temperature
range may damage it.
technical and service
If you have any questions and the product documentation does not provide the relevant information, please contact your local technical office. Or log on to the LLYNAV website ( http://www. a llynav.cn ) to inquire and download the latest version of the product and related technical information, or call the national service hotline: 400-1698-003/021-61200180 to contact us, we Will be happy to serve you.
Security Information
Before using the R51 receiver product, please ensure that you have carefully read and understood this user guide and safety requirements.
Product introduction
Introduction
The R30 Bei Dou/GNSS receiver is a multi-functional high-precision RTK Bei Dou/GNSS receiver independently developed by Lian Shi Navigation Co., Ltd.. Built-in high-precision OEM board, full Netcom 4G module, Ethernet communication interface, high-speed data storage module, CAN data communication, etc., each functional module can be customized according to customer needs. This receiver has industrial grade design, strong anti- interference ability and high stability, and is widely used in precision agriculture, driving test and driving training, surveying and mapping engineering, mechanical control, high-precision vehicle positioning and navigation, geographic information, deformation monitoring and other industries.
Product Features
-
Using high-precision positioning and orientation GNSS technology, it supports 432
channels.
GPS: L1/L2
GLONASS L1/L2
Galileo E1/E5b
BDS: B1 / B2 -
Built-in boards are optional and coecum UM482 boards or dream core MXT906B boards.
-
The output rate of the 9-axis gyroscope is adjustable from 0.1 to 200 Hz, and the attitude measurement accuracy is static 0.05 degrees and dynamic 0.1 degrees
-
Support Bluetooth wireless access, convenient for user configuration
-
Support 4G full Netcom
-
Up to 20HZ data update rate
-
IP67 waterproof rating
-
Compact internal shock absorption technology, strong adaptability to vibration and shock, and high reliability
-
Built-in solar controller, can connect 4~ 5A 21.6~ 26 V solar panel
-
The solar panel battery can use lead-acid battery, gel battery
-
Optional built-in 9.75Ah lithium battery
Product parameter table
Displacement measurement
Static relative positioning accuracy| Horizontal ±(2.5mm+0.5ppm)RMS
Vertical ±(5mm+0.5ppm)RMS
Dynamic relative positioning accuracy| Horizontal ±(8mm+1ppm)RMS
Vertical ±(15mm+1ppm)RMS
sampling interval| 0s~24h
Upload interval| 0s~24h
output signal| NB/4G Cat1, PORT (nine-pin aviation plug)
Operating mode| MODE0 debug mode
MODE1 Displacement measurement mode
Data Format| Support RTCM32 and real-time dynamic upload of raw observation
data
Physical Dimensions and Electrical Characteristics
Input voltage| 9~26V DC (standard adapt to 12V DC)
Power consumption| ≤ 4W (typ.)
physical size| 196.5×196.5×129.5mm
weight| 1.3kg (without battery)
Lithium Ion Battery| 9.75Ah ( 70.2Wh ) optional
Solar Controller| maximum input voltage of 26V is allowed, and a solar panel
with 4~ 5A 21.6V no-load voltage or close to this value is recommended
Environmental indicators
Installation method| Standard observation pier, cast-in-place concrete pier,
steel structure, etc.
Operating temperature| -40~+60 ℃
User Interface
Front
Bottom panel
| Power light: red and blue flash alternately when power on
---|---
| Differential light red: (monitoring mode is disabled)
| 4G light red: 4G is not online, flashes every 5s , and flashes every 1s
after going online.
| Differential data status light red (monitoring mode is disabled)
| Storage light red : (Monitoring mode is disabled)
| Bluetooth light is red : the Bluetooth is not connected and flashes once for
3 s, and the Bluetooth flashes twice for 1 s after the Bluetooth is connected.
SIM card : Use a NANO SIM card, with the chip facing down
- PORT nine -pin aviation plug: used for 12V DC power input and one R S232 communication serial port.
Accessories
This chapter provides accessory information. Before starting the installation, make sure that all accessories used in the project meet specifications and standards.
Configuration List
name | quantity | picture |
---|---|---|
R 51 Universal Receiver (Host) | 1 pcs | ![Product |
introduction](https://manuals.plus/wp-content/uploads/2023/01/AllyNav-R51
-GNSS-Receiver-User-Manual-3.png)
Nine core aviation plug power cord| 1 pcs|
Nine core aerial plug setting line| 1pcs|
Data line interface definition
nine -core aerial plug setting line mainly includes 1 DC power port, 2 R S232 serial ports The nine-core aviation plug power cord includes a solar power supply interface and a battery power supply interface
Defined as follows
R51 universal receiver P ORT nine-core aviation plug pin definition
Aviation PIN
sequence (male)
| definition
---|---
1| POWER+
2| POWER –
3| SOLAR +
4| L EAC BAT
5| R S232 RX
6| RS232TX
7| G ND
8| G ND
9| PON
Nine-core aerial plug power cord P IN pin definition
Aviation PIN sequence (female) | definition |
---|---|
1 | (empty ) |
2 | (empty ) |
3 | SOLAR + (Solar Anode) |
4 | B AT+ (battery positive) |
5 | (empty ) |
6 | (empty ) |
7 | SOLAR- (Solar Negative ) |
8 | B AT- (battery negative |
electrode)
9| (empty )
Nine-core aerial plug setting line P IN pin definition
Aviation PIN sequence (female) | definition |
---|---|
1 | DC 12V positive |
2 | D C 12V negative pole |
3 | COM RS232B |
4 | (empty ) |
5 | C ONFIG RS232 B |
6 | C ONFIG RS232A |
7 | COM RS232A |
8 | (empty ) |
9 | (empty ) |
PORT RS232: Various parameters of the receiver can be configured through the serial port tool, the default baud rate is 115200 .
Overview of the configuration instruction set
System debugging instructions
S ET UART CONFIG| Open system configuration
M ODE0| Switch to debug mode
M ODE1| Switch to monitoring work mode
C ONCOM12| Connect to G NSS board debug interface
C ONCOM13| Connect the gyroscope debugging interface
C ONCOM14| Connect 4G network module debugging interface
C ONCOM15| System debugging interface and Bluetooth transparent transmission
C ONCOM25| Transparent transmission between G NSS board and Bluetooth module
B ATTIME60| Set the time interval for uploading power information, once every
60 seconds; the setting range is 0 ~ 255 seconds
S AVE LIST| save system configuration
G NSS board debugging instructions
U NLOGALL| Turn off all outputs of the G NSS board
L OG RANGEB ONTIME 1| Hz raw observation data in binary format
L OG RANGEA ONTIME 1| Output 1 Hz raw observation data in ASCII format
LOG GPSEPHEMB ONTIME 300| GPS ephemeris in binary format , every 300 seconds
LOG BD2EPHEMB ONTIME 300| DS ephemeris in binary format , every 300 seconds
LOG GLOEPHEMERISB ONTIME 300| GLO ephemeris in binary format , every 300
seconds
LOG GPSEPHEMA ONTIME 300| Output GPS ephemeris in ASCII format , every 300
seconds
M ODE ROVER| Converting from Base Mode to Rover Mode
L OG GPGGA ONTIME 0.5| Output G PGGA statement 2 Hz
MASK 15| Set the satellite altitude cutoff angle to 15 degrees
SAVECONFIG| Save the board configuration
Gyro debugging instructions
41 6C 6C 79 02 FF AA 03 03 00| Modify the output frequency of the gyroscope
with ID number 0 2 to 1 Hz (H EX send )
41 6C 6C 79 02 FF AA 0 4 0 6 00| Modify the baud rate of the gyroscope serial
port with ID number 0 2 to 115200 (sent by H EX )
41 6C 6C 79 02 FF AA 2D FF 00| Modify the ID number of the gyroscope whose ID
number is 0 2 to FF ; allow the modification range of 0 0 ~ FF (H EX send)
4G network debugging instructions
SETG3CONFIG | Turn on 4G configuration state
SETG3MODE0 | 4 G module switches to debug mode
SETG3IP0192.168.1.100 | Set the TCP server IP to 1 92.168.1.100
SETG3PORT01002 | Set the TCP server port to 1002
SETG3MODE2 | Set 4G as TCP transparent transmission working mode
SETG3QUIT | Save and exit the 4G configuration state, and the 4G
configuration parameter information will pop up
Detailed explanation of gyroscope configuration instructions: First adjust the display interface to H EX display, the ID of the gyroscope can be queried in the data 4 1 6C 6C 79 __ field spit out from the serial port . Commands are sent in hex ID number of the gyroscope module whose ID is 02 to FF. The command is as follows : Input example: 41 6C 6C 79 02 FF AA 2D FF 00 The red font is the gyroscope ID; the blue font is the modification ID option; the green font is the ID to be written Modify the frequency of the serial port output data of the device whose gyroscope ID is 02 to 50 Hz. The command is as follows : Input example: 41 6C 6C 79 02 FF AA 03 08 00 The red font is the gyroscope ID; the blue font is the modification frequency option; the green font represents the specific output frequency (08=50HZ) For example , the command to modify the serial port baud rate of the device whose gyroscope ID is 02 is 115200 is as follows: Input example: 41 6C 6C 79 02 FF AA 0 4 0 6 00 The red font is the gyroscope ID; the blue font is the option to modify the baud rate; the green font represents the baud rate to be set (0 6 = 115200 )
Notice:
- Before preparing to modify the parameters of the G NSS board , gyroscope, and 4G network module, it is necessary to send the system debugging command, connect to the corresponding debugging interface, and then send the configuration command of the corresponding module.
- If you want to set the parameters of each module of the system through Bluetooth, you need to send an instruction to connect to the corresponding debugging interface first; for example, CONCOM25/CONCOM35/CONCOM45 can be configured with GNSS board/gyroscope/ 4G network module respectively.
- After the module parameter configuration is completed, the system debugging command needs to be sent again, and the device can be switched to the MODE1 working mode before it can work normally.
- System debugging and each module have corresponding save configuration commands. After debugging, you need to send save commands, otherwise the corresponding configuration will be invalid after power off.
data protocol
Gyroscope Data Protocol
Time output:
0x55 _ | 0x50 _ | Y Y | M M | D D | H H | M M | D D | M SL | M SH | SUM _ |
---|
YY : year, year 20YY
MM : month
DD : day
HH : Hour
MM : points
SS : seconds
MS : milliseconds
Millisecond calculation formula:
MS=((MSH <<8)|MSL)
Sum=0x55+0x50+YY+MM+DD+HH+MM+SS+MSL+MSH
Acceleration output:
0x55 _ | 0x51 _ | Ax L | AxH | A y L | A y H | A zL | A zH | TL | TH | SUM _ |
---|
Calculation method:
ax=(( AxH <<8)| AxL )/3276816g (g is the acceleration of gravity, preferably
9.8m/s2)
ay=(( AyH <<8)| AyL )/3276816g (g is the acceleration of gravity, preferably
9.8m/s2)
a z =(( AzH <<8)| AzL )/32768*16g (g is the acceleration of gravity,
preferably 9.8m/s2)
Temperature calculation formula:
T=((TH <<8)|TL) /100 ℃ Checksum:
Sum=0x55+0x51+AxH+AxL+AyH+AyL+AzH+AzL+TH+TL illustrate:
- The data is sent in hexadecimal , not ASCII .
- Each data is divided into low byte and high byte and transmitted in turn, and the two are combined into a signed short type of data.
For example , the X- axis acceleration data Ax , where AxL is the low byte,
AxH is the high byte. The conversion method is as follows:
Assuming Data is actual data, DataH its high byte part, DataL for its low byte
part, So:
Data=(short) ( DataH <<8| DataL ). Here we must pay attention to DataH Need to
cast to a signed first of the short type of the number is shifted later, and
the data type of the Data is also a signed short type. This is how negative
numbers can be represented
Angular velocity output:
0x55 | 0x52 | wxL | wxH | wyL | wyH | wzL | wzH | TL | TH | SUM |
---|
Calculation method:
wx =(( wxH <<8)| wxL )/327682000( ° /s)
wy =(( wyH <<8)| wyL )/327682000( ° /s)
wz =(( wzH <<8)| wzL )/32768*2000( ° /s)
Temperature calculation formula:
T=((TH<<8)|TL) /100 ℃
Checksum:
Sum=0x55+0x52+wxH+wxL+wyH+wyL+wzH+wzL+TH+TL
Angle output:
0x55 | 0x53 | RollL | RollH | PitchL | PitchH | YawL | YawH | TL | TH | SUM |
---|
Calculation method:
Roll angle ( x axis) Roll=(( RollH <<8)| RollL )/32768180( ° )
Pitch angle ( y – axis) Pitch=(( PitchH <<8)| PitchL )/32768180( ° )
Yaw angle ( z axis) Yaw=(( YawH <<8)| YawL )/32768*180( ° )
Temperature calculation formula:
T=((TH<<8)|TL) /100 ℃
Checksum:
Sum=0x55+0x53+RollH+RollL+PitchH+PitchL+YawH+YawL+TH+TL
Note:
- The coordinate system used for attitude angle settlement is the northeast sky coordinate system, and the module is placed in the positive direction , as shown in the figure below.is the X axis, forward is the Y axis, and upward is the Z axis. The rotation order of the coordinate system when Euler angles represent the attitude is defined as zyx, that is, rotate around the z -axis first, then around the y -axis, and then around the x -axis.
- Although the range of the roll angle is ± 180 degrees, in fact, because the coordinate rotation order is ZYX , the attitude is expressed. When , the range of the pitch angle (Y- axis ) is only ± 90 degrees, and when it exceeds 90 degrees, it will change to less than 90 degrees, and at the same time Make the angle of the X axis greater than 180 degrees. For detailed principles, please refer to Baidu’s Euler angle and attitude representation.
- Since the three axes are coupled, they will show independent changes only when the angle is small, and the attitude will be changed when the angle is large.
The angle will be coupled to change, for example, when the Y- axis is close to 90 degrees, even if the attitude only rotates around the Y – axis, the angle of the X- axis It will also change greatly, which is an inherent problem of the Euler angle representing the attitude.
Magnetic field output:
0x55 | 0x54 | HxL | HxH | HyL | HyH | HzL | HzH | TL | TH | SUM |
---|
Calculation method:
Magnetic field ( x – axis) Hx =(( HxH <<8)| HxL )
Magnetic field ( y – axis) Hy =(( HyH <<8)| HyL )
Magnetic field ( z – axis) Hz = (( HzH <<8)| HzL )
Temperature calculation formula:
T=((TH<<8)|TL) /100 ℃
Checksum:
Sum=0x55+0x54+HxH+HxL+HyH+HyL+HzH+HzL+TH+TL
Voltage Data Protocol Data Protocol
Voltage data is output in the form of Chinese characters plus decimal values like:
Solar 12.0, lead-acid battery 8.7, lithium battery 8.4, USB1.5, temperature 36.6
Note:
The charging process of the solar controller is as follows Solar power allows
a maximum input voltage of 26V, and a solar panel with a no-load voltage of
21.6V or close to this value is recommended.
When the solar voltage is greater than 17.2V, the battery starts to be
charged. When the battery voltage exceeds 10.6V, the controllable switch is
turned on, the equipment starts to work, and the internal lithium battery is
charged at the same time.
voltage of the built-in lithium battery is greater than 6.2V , the device
starts to work. When there is no built-in lithium battery, and the battery
voltage exceeds 10.6V , the device can be turned on to work.
Directive configuration example
Example: Send commands through the RS232 serial port to set the G NSS board to output 10 Hz GPGGA text, modify the gyroscope output frequency to 10 Hz; modify the 4G network TCP server address and port number; modify the voltage upload time to 60 seconds1 times; the order of sending commands is as follows.
SET UART COFIG
MODE 0
CONCOM12
LOG GPGGA ONTIME 0.1
SAVECONFIG
CONCOM13
//For example, the gyroscope ID is 02 (the following commands are sent in the
form of HEX)
41 6C 6C 79 02 FF AA 03 06 00
CONCOM14
SETG3CONFIG
SETG3IP0 192.168.1.100
SETG3PORT0 8001
SETG3MODE2
SETG3QUIT
B ATTIME60
MODE1
SAVE LIST
The command to configure the above parameters using Bluetooth is as follows (first need to connect to Bluetooth, and send the following commands from the Bluetooth serial port) .
SET UART COFIG
MODE 0
CONCOM25
LOG GPGGA ONTIME 0.1
SAVECONFIG
CONCOM35
//For example, the gyroscope ID is 02 (the following commands are sent in the
form of HEX)
41 6C 6C 79 02 FF AA 03 06 00
CONCOM45
SETG3CONFIG
SETG3IP0 192.168.1.100
SETG3PORT0 8001
SETG3MODE2
SETG3QUIT
B ATTIME60
MODE1
SAVE LIST
Equipment FAQ
fault phenomenon | Failure Analysis Cause | Solution |
---|---|---|
Can’t find bluetooth ID | phone is too far from the receiver or the ID is not | |
fully loaded | mobile phone is close to the receiver to search again for the |
VBluetooth device whose ID number is the device S N number
4G does not upload data| The 4G module IP or port configuration is wrong, and
the 4G SIM card is installed in the wrong direction device is in MODE0 debug
mode| Reconfigure the 4G module IP or port, check whether the SIM card is
installed correctly, and adjust the device to MODE1 working mode.
Device light is off| The power cord is loose or reversed| Check whether the
power cord is reversed and tightened
The output data is garbled or all dots| Incorrect baud rate setting| Check
that the baud rate set by the computer serial port receiving program is
consistent with the baud rate of the device CONFIG .
FCC Statement
FCC Statement
Any Changes or modifications not expressly approved by the party responsible for compliance could void the user’s authority to operate the equipment. This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions:
- This device may not cause harmful interference, and
- This device must accept any interference received, including interference that may cause undesired operation.
FCC Radiation Exposure Statement:
This equipment complies with FCC radiation exposure limits set forth for an
uncontrolled environment .This equipment should be installed and operated with
minimum distance 20cm between the radiator& your body.
Note : This equipment has been tested and found to comply with the limits
for a Class B digital device, pursuant to part 15 of the FCC Rules. These
limits are designed to provide reasonable protection against harmful
interference in a residential installation. This equipment generates, uses and
can radiate radio frequency energy and, if not installed and used in
accordance with the instructions, may cause harmful interference to radio
communications. However, there is no guarantee that interference will not
occur in a particular installation. If this equipment does cause harmful
interference to radio or television reception, which can be determined by
turning the equipment off and on, the user is encouraged to try to correct the
interference by one or more of the following measures:
- Reorient or relocate the receiving antenna.
- Increase the separation between the equipment and receiver.
- Connect the equipment into an outlet on a circuit different from that to which the receiver is connected.
- Consult the dealer or an experienced radio/TV technician for help.
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