Description
MNS620 Micro Inertial/GNSS Integrated Navigation systems – MEMS Inertial Devices and Systems
Applications
- Unmanned Helicopters & Light Helicopters
- UAV & AGV
- Platform Stabilization
- Robitic Control & Machine State Monitoring
- Vessel Applications
- Inertial Navigation Systems
Parameter | MNS620 | Notes | |
Heading | Range | ±180° | |
Accuracy | 1°/60s | ||
Resolution | 0.01° | ||
Attitude | Range: Roll, Pitch | ±180°, ±90° | |
Dynamic Accuracy | 1°/60s | ||
Resolution | 0.01° | ||
Anaular Rate | Range: Roll, Pitch, Yaw | ±300°sec | Extendable |
±500°sec | High Full Scale | ||
Zero Absolute Error | < 0.1°/sec | ||
Zero Instability | < 2°/hr | ||
Resolution | 0.005°/sec | Typical Allan Variance | |
ARW | <0.15°/√h | ||
Acceleration | Range: X, Y, Z | ±15g | |
Bias Stability | <0.5mg | Overworking Temperature | |
Resolution | 0.1(mg) | ||
Bandwidth | Sensor Bandwidth | 60Hz | Extendable, 5~480Hz |
Environments | Shock survival in run | 2000g@1 ms | |
Shock survival power off | 10000g@0.1ms | ||
Vibration Operational | 10g rms | 20Hz~2kHz, Random | |
Operating Temperature | -40°C ~85°C | -55°C~125°C | |
Protection Level | IP66 | ||
Power Consumption | Input Voltage | 11-13DC V | Voltageclamp >15.0V |
Size | 70mm x 54mm x 39mm | ||
Weight | < 250g | ||
Interface | DB15 | ||
All values are typical at +25°C, +12Vdc unless otherwise statement. |
Structure (unit: mm)
1 | VCC | Power(+12V) |
2 | GND | Power Ground |
3 | R1 + | RS422 Positive Input (Interface 1) |
4 | R1- | RS422 Negative Input (Interface 1) |
5 | T1- | RS422 Negative Output (Interface 1) |
6 | T1 + | RS422 Positive Output (Interface 1) |
7 | GND1 | RS422 Ground(Interface 1) |
8~9 | NC | No Connection |
10 | R2+ | RS422 Negative Output(lnterface2) |
11 | R2・ | RS422 Negative Output(lnterface2) |
12 | T2- | RS422 Positive lnput (lnterface2) |
13 | T+ | RS422 Positive Input(lnterface2) |
14 | GND2 | RS422 G round (1 nterface2) |
15 | Shield | Shield Ground |