GSY-MINS-210/230 MEMS Inertial Navigation System
Introduction
GSY-MINS-210/230 MEMS Inertial Navigation System uses a high-precision, high-dynamic GPS receiver as a satellite signal sensor. It adopts carrier phase differentiation technology and fast calculation of the ambiguity of the whole circle, which can accurately calculate the azimuth angle of the carrier＊s movement. When GPS signals interfere, the system can still output high-precision data by maintaining the inertial measurement unit for a period of time.
Features
GSY-MINS-210/230 MEMS Inertial Navigation System overcomes the deficiency of a single device, gives full play to the GPS high precision, with no accumulation error, no drift, low price and inertial products good dynamic performance, strong anti-interference ability. Without the need of external signal source, it is able to work and improve the overall attitude measurement accuracy, navigation accuracy and real-time tracking performance of the system. The proof in the land, sea and air a variety of environmental tests, heading accuracy of 0.1 degrees, roll and pitch accuracy 0.05 degrees, and effectively overcome the drift angle of heading error. It is multi system compatible and complement each other, mutual backup all-weather high reliability azimuth measurement products. Especially for satellite communication vehicle, meteorological radar vehicle, warship, expedition ship, airship, UAV, fire control system, command and control system, weapon aiming system, have very strong competitiveness.
Applications
GSY-MINS-210/230 MEMS Inertial Navigation System can provide horizontal attitude, heading attitude and other information, longitude, latitude, altitude, positioning information, the 3D acceleration, angular velocity inertial measurement information andetc. By extending the range of the mileage meter and the height of the barometer, it further improves the accuracy and applicability of the system and it can be widely used in unmanned aerial vehicles, vehicle navigation, aviation and platform stability control and other fields.
Specifications
| Systematic Name | GSY-MINS-210 | GSY-MINS-230 |
| Performance Indicators | ||
| Heading | ≒1.0 deg (1考) | ≒0.3 deg (1考) |
| Horizontal Attitude (Roll and Pitch) | ≒0.5 deg (1考) | ≒0.2 deg (1考) |
| Horizontal Position | 2.5 m CEP | 2.5 m CEP |
| Elevation | 4 m CEP | 4 m CEP |
| Speed | ≒0.2 m/s (1考) | ≒0.1 m/s (1考) |
| Gyroscope | ||
| Range | ㊣100 deg/s | ㊣400 deg/s |
| Bias Stability | ≒0.05 deg/s | ≒10 deg/h |
| Bias Repeatability | ≒0.05 deg/s | ≒10 deg/h |
| Accelerometer | ||
| Range | ㊣10 g (customizable) | ㊣10g |
| Bias Stability | ≒0.1 mg | ≒0.1mg |
| Bias Repeatability | ≒0.2 mg | ≒0.2mg |
| GNSS | ||
| GNSS Features | 16 Channel, GPS L1 Frequency Point | 16 Channel GPSL1, BD B1 |
| Positioning Time | ≒60 s | ≒60 s |
| Typical Recapture Time | ≒10 s | ≒10 s |
| Interface Features | ||
| Voltage | 9~36Vdc | 9~36Vdc |
| Power Consumption | ≒3.5W@12VDC | ≒4W@24VDC |
| Electrical Interface | RS232/RS422 | RS422 |
| Data Update Rate | 100Hz@115, 200bps | 100~200Hz |
| Operating Environment | ||
| Operating Temperature | -40∼C~+85∼ C | |
| Storage Temperature | -55∼C~+85∼ C | |
| Vibration | 6g@20~2000Hz | |
| Shock | 30g, 11ms, 1/2 Sine | |
| Physical Property | ||
| Physical Size | 68.8℅68℅70 mm | 86.8℅68℅87 mm |
| Weight | ≒500g | ≒500g |
FAQ:
1. What are the quotation methods?
If you have DHL or Fedex account, we can quote EXW price, otherwise CIF or FOB price.
2. Are there any discounts?
After we submit the sample price, if more quantity is needed, we will quote the bulk price.
3. How long will it take to deliver the goods after placing the order?
For sensors, parts and modules: in stock-one week; no stock-2-4 weeks; For systems, generally, 8-12 weeks.
4. How to deal with the quality problems?
After confirming that the product has quality problems, we will replace it for you free of charge in the shortest possible time.
If interested in MEMS Inertial Navigation System, pls contact us: info@joinsunny.cn
