Negotiable
The date of payment from buyers deliver within days
Beijing
Long-term effective
2020-03-24 11:43
195
Company Profile
HongKong Liocrebif Technology Co., LtdBy certification [File Integrity]
Contact: liocrebif(Mr.)
Email:
Telephone:
Phone:
Area: Beijing
Address: Beijing
Website: http://www.liocrebif.com/ http://liocrebif.xskqc.com/
unit price:Negotiable
unit price:Negotiable
unit price:Negotiable
unit price:Negotiable
unit price:Negotiable
unit price:Negotiable
Key Features
● Pure inertial positioning accuracy (CEP)
≤ 100m/min
● Heading accuracy (low dynamic)
≤ 1° (the magnetic heading accuracy in non-magnetic environment)
● Heading accuracy (high dynamic)
≤ 1°
● Attitude accuracy
≤ 0.2°
● Three-axis MEMS gyros
● MEMS accelerometer
● Volume 68mm×55mm×33mm
● Weight < 150g
● Power < 3W
● Communication interface
RS422/232
Applications
● Automatic control equipment: unmanned aerial vehicles (UVA), robots, precision agriculture, automatic guided vehicle (AGV), port logistics automation
● Communication in moving, survey in moving
● Antenna servo stabilized platform
Customized Service
● Customization is available
GNSS/INS MEMS Integrated Navigation System Designed for Performance
LKF-MN300 GNSS/INS integrated navigation system is a high-performance MEMS measurement equipment for attitude and position, which can be used in navigation, control, dynamic measurement and other fields. The LKF-MN300 integrates a high-performance MEMS inertial measurement unit (IMU), a GNSS receiver and a variety of other navigation sensors in an independent structure. The IMU uses three-axis high-precision MEMS gyroscope to sense the angular motion of the carrier, which outputs digital signals proportional to the angular velocity of the carrier. Three MEMS accelerometers are orthogonally configurated to sense the linear acceleration of the carrier. The gyroscopes and accelerometers selected by IMU represent the leading level of inertial devices in MEMS technology, which ensure that the integrated navigation system can maintain high navigation accuracy even when the signal of GNSS is invalid. At the same time, strict technology is adopted to ensure that the product can still accurately measure the angular motion and linear motion parameters of the carrier in harsh environment. LKF-MN300 GNSS/INS integrated navigation system is a high precision and high reliability solution.
Designed for Cost-effective and Stability
Compared with other gyroscopic technologies, MEMS has a significant cost advantage. At the same time, LKF-MN300 integrates three-axis magnetic sensor, barometric altimeter and GPS/BDII dual-mode satellite navigation receiver. The measurement accuracy of inertial devices is guaranteed by multi-compensation technology. Two different but complementary navigation modes, Global Navigation Satellite System (GNSS) and Inertial Navigation System (INS), are integrated by using the optimal estimation method. INS have the advantages of full autonomy and can provide stable and continuous navigation information at high frequency. Combining the GNSS advantage of high position accuracy, LKF-MN300 can output stable and continuous three-dimensional navigation information under the condition that satellite signals are not available, which guarantees the optimal navigation performance under dynamic conditions.
Ideal for precision agriculture and port logistics automation. LKF-MN300 provides a high precision and high reliability, and has a significant cost advantage.
LKF-MN300 GNSS/INS Integrated Navigation System | ||||||
Horizontal Position Accuracy (RMS) | ||||||
Position in Integrated Navigation Mode |
15m |
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Velocity in Integrated Navigation Mode |
0.15m/s |
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Attitude Accuracy (RMS) | ||||||
|
Heading Accuracy |
Pitch Accuracy |
Roll Accuracy |
|||
With GNSS (alignment accuracy is related to carrier maneuver conditions) |
0.8° |
0.15° |
0.15° |
|||
GNSS Single Loss for 10s |
0.9° |
0.2° |
0.2° |
|||
IMU Performance | ||||||
Gyro Performance |
Accelerometer Performance |
|||||
Gyro Type |
MEMS |
Accelerometer Type |
MEMS |
|||
Output Range |
±400°/s |
Output Range |
±10g |
|||
Bias Repeatability |
20°/h (1σ) |
Bias Repeatability |
1mg (1σ) |
|||
Bias Stability |
5°/h (1σ) |
Bias Stability |
0.3mg (Allan) |
|||
Scale Factor |
300ppm (1σ) |
Scale Factor |
500ppm (1σ) |
|||
Non-orthogonality |
0.05° |
|||||
Satellite Receiver Specifications |
Magnetic Specifications |
|||||
Working Frequency |
L1/B1 |
Range |
6Gauss |
|||
Cold Start Time |
60s |
Noise |
10μGauss |
|||
Hot Start Time |
10s |
Scale Factor |
1000ppm |
|||
Position Accuracy |
10m (RMS) |
|||||
Velocity Accuracy |
0.1m/s (RMS) |
|||||
Time Synchronization Accuracy |
20ns |
|||||
Communication Interface | ||||||
Serial RS-232 Port |
1 |
|||||
Serial RS-422 Port |
1 |
|||||
Data Update Rate | ||||||
GNSS Update Rate |
5Hz |
|||||
IMU Update Rate |
1KHz |
|||||
INS Computing Rate |
Up to 1KHz |
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