Low Cost Single Antenna MEMS Integrated Navigation System

ER-GNSS/MINS-07
1.High reliability and low cost MEMS IMU. The working temperature is -40℃~+80℃.
2.Built-in dual-band full-system single-antenna positioning GNSS module, supporting single-antenna high-precision positioning and velocity measurement.
3.The system can provide accurate integrated navigation information, attitude up to 0.1°, heading 0.1°.

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Introduction

ER-GNSS/MINS-07 Low Cost Single Antenna MEMS Integrated Navigation System

Introduction
ER-GNSS/MINS-07 is equipped with a highly reliable MEMS IMU and integrates a single-antenna full-system multi-frequency positioning satellite module. It is a low-cost single-antenna integrated navigation system.
Equipped with a integrated navigation fusion algorithm, it can provide continuous, accurate and reliable positioning, attitude, and speed information, with attitude up to 0.1° and heading 0.1°.
It uses a low-cost MEMS inertial measurement unit (IMU), internally integrated with a three-axis MEMS gyroscope and accelerometer, and a -40℃~+80℃ full-temperature range temperature compensation algorithm, which greatly reduces costs while ensuring core performance.
Different from the complex structure and cost of traditional dual-antenna solutions, ER-GNSS/MINS-07 adopts a single-antenna full-system dual-frequency design to achieve high-precision positioning and speed measurement.
The precision aluminum alloy shell has high reliability and adapts to harsh environments. It has a variety of communication interfaces and provides standardized user communication protocols to meet aviation, land and other applications.

Feature
The system can provide accurate combined navigation information, with attitude up to 0.1° and heading 0.1°.
High reliability and low-cost MEMS IMU. Operating temperature -40℃~+80℃.
Built-in single-antenna full-system multi-frequency GNSS module, supporting single-antenna high-precision positioning and speed measurement.
Multiple data interfaces, easier to install and use, supporting RS422/RS232 and CAN.
Precision aluminum alloy housing, high reliability, can be widely used in land and aviation.

Application areas
UAV, flight recorder, ADS

Specification
1.System parameter

ER-GNSS/MINS-07
Roll & Pitch	0.1°
Heading(dynamic)	0.2°
Heading(magnetic compass)	0.8°
Speed accuracy	0.02 m/s
RTK 30 sec outage	Roll & Pitch	Heading
	0.05°	0.1°
	Position (X/Y)	Altitude (Z)
	1.0 m	0.5 m
RTK 60 sec outage	Roll & Pitch	Heading
	0.1°	0.2°
	Position (X/Y)	Altitude (Z)
	15 m	3 m
Alignment Time	3 min

2.Sensor parameter

IMU Performance
Item	Value	Unit
Gyro range	±125、500、1000、2000	deg/s
Gyro ARW	0.21	°/ √h
Gyro sensitivity	4.37 @FS=±125 17.5@FS=±500 35.0@FS=±1000 70.0@FS=±2000	mdps/LSB
Gyro Bias instability	3	°/h
Acc Range	±2、4、8、16	g
Acc sensitivity	0.061@FS=±2 0.122@FS=±4 0.244@FS=±8 0.488@FS=±16	mg/LSB
Acc Bias stability	0.1	mg

Barometer
Parameter	value	Unit
Range	10~1200	mbar
Accuracy 25℃, 750mbar	±1.5	mbar
Error band, -20℃~+85℃, 450~1100mabr	±2.5	mbar
Temperature	-40℃~+85℃	\
Long-term stability	±1	mbar/year

Magnetometer
Range	±2	gauss
Sensitivity	11000	LSB/G
Temperature Sensor Sensitivity	14	LSB/℃
Field Resolution	1.2	mgauss
X-Y-Z Orthogonality	90±1	Degree

Satellite Receiver
Supported Navigation System	GPS/BDS-2/BDS-3/GLONASS/Galileo/QZSS/SBAS/IRNSS
ANT Frequency	GPS: L1C/A,L2P, L2C, L5 BDS-2: B11, B21, B31 BDS-3: B11, B3l, B2a GLONASS: G1,G2 Galileo: El,E5b, E5a QZSS: L1C/A, L2C, L5 SBAS: L1C/A, L5 IRNSS*: L5
Position Accuracy (RMS)	Single point positioning	Horizontal	1.5m
		Altitude	3m
	RTK	Horizontal	±(8+10-6×D)mm D represents the baseline length(mm)
		Altitude	±(15+10-6×D)mm D represents the baseline length(mm)
Time accuracy (RMS)	20ns
Speed accuracy (RMS)	0.02m/s
First positioning time	24s

Power ＆ Interface
Supply Voltage	5~12V
Supply Consumption	3W
Interface	1-Way RS422 or 1-Way RS232 and 1-Way CAN and 1-Way TTL (NMEA output and RTCM input)
Environment
Operate Temp	-40℃~+80℃
Storage Temp	-55℃~+95℃
Dimension
Dimension	40mm40mm45mm