Headquarters Address: Building 3, Science and Technology Innovation Park, No. 311 Yanxin Road, Huishan District, Wuxi City
Email: sales@witlink.cn
Phone: 0510-83880511
Website: www.witlink.cn
Main characteristics：INS300 is an autonomous navigation positioning and orientation system that is not affected by external environmental interference and has the capability of autonomous navigation positioning and orientation. It can be used in navigation guidance, attitude measurement, and control systems for missiles, ships, underwater robots, and underground engineering machinery vehicles. It is a key component of navigation control systems and is suitable for high-precision navigation control system applications.
Product Introduction
INS300 is an autonomous navigation positioning and orientation system that is not affected by external environmental interference and has the capability of autonomous navigation positioning and orientation. It can be used in navigation guidance, attitude measurement, and control systems for missiles, ships, underwater robots, and underground engineering machinery vehicles. It is a key component of navigation control systems and is suitable for high-precision navigation control system applications.
INS300 can provide real-time information on the three-dimensional position, attitude, angular velocity, acceleration, and other aspects of the carrier. INS300 adopts high-precision fiber optic gyroscope as the core inertial measurement unit, with high accuracy, reliability and stability. The INS300 can accurately self locate the north for initial alignment, and can also introduce initial attitude information from the outside world for navigation data calculation.
INS300 supports external odometer information for assistance, and can also integrate satellite navigation information for data fusion. With the help of new generation precise calibration technology and multi-sensor data fusion technology, the reliability, accuracy, and dynamism of the system are greatly improved. The INS300 adopts the inertial navigation/satellite tight coupling algorithm and has functions such as dynamic base alignment, inertial navigation/satellite integrated navigation, autonomous zero velocity correction, and autonomous calibration.
Main characteristics
◆ High precision fiber optic gyroscope
◆ Full temperature compensation throughout the process
◆ Unique Strapdown Attitude Algorithm and Kalman Filter
◆ Can be combined with satellite navigation and odometer
◆ Can work normally in harsh environments
◆ Anti vibration impact and anti electromagnetic interference
◆ Strong autonomy, good reliability, and high cost-effectiveness
Application area
◆ Satellite tracking
◆ Drilling equipment measurement and control
◆ Marine survey instrument
◆ Antenna stabilization platform
◆ Underwater/Underwater Navigation and Benchmarking
◆ Aviation and unmanned aerial vehicles
◆ Ship navigation and attitude measurement
◆ Mining and automated farming
◆ Vehicle mounted and launch devices
◆ Navigation and control of vehicles
◆ Tracking of high-speed trains and containers
Index
Integrated navigation indicators (effective satellite navigation data, dual antenna high-precision satellite navigation baseline length of 4m)
Number | Project indicators | Index |
1 | Self seeking North Accuracy (°) | ≤0.06*Secant Latitude |
2 | Azimuth accuracy (°) | ≤0.02 |
3 | Attitude angle accuracy: (°) (pitch, roll) | ≤0.01 |
4 | Speed accuracy (m/s) | ≤0.03 |
5 | Position accuracy (m) | 2 |
6 | Position accuracy (m) (RTK positioning) | 0.02 |
7 | Range of azimuth measurement (°) | ±180 |
8 | Range of elevation measurement (°) | ±90 |
9 | Rolling measurement range (°) | ±180 |
Technical specifications of accelerometer
Number | Parameter | Unit | Index |
1 | Range | g | ±20 |
2 | Deviation value | mg | ≤3 |
3 | Scale factor | mA/g | 0.8-1.2 |
4 | Second order nonlinearity | ug/g2 | ≤50 |
5 | Deviation temperature coefficient | ug/℃ | ≤50 |
6 | Scale factor temperature coefficient | ppm/℃ | ≤80 |
7 | Bias stability | ug | ≤50 |
8 | Scale factor repeatability | ppm | ≤80 |
9 | Second-order nonlinear repeatability | ug/g2 | ≤30 |
10 | Natural frequency | Hz | ≤800 |
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