| Customization: | Available |
|---|---|
| Accuracy: | <1mm |
| Horizontal Line: | 1 |
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| System accuracy | |||
| Pure inertial alignment accuracy | North finding accuracy | ≤0.05°×secφ | (RMS) |
| Attitude accuracy | ≤0.003° | (RMS) | |
| Pure inertia retention accuracy | Heanding angle | ≤0.01° | (RMS,1h) |
| Attitude angle | ≤0.005° | (RMS,1h) | |
| Position | ≤1nmile/h | (CEP50%) | |
| Velocity | ≤0.5m/s | (RMS,1h) | |
| INS+GNSS integrated accuracy | Heading | ≤0.02° | (RMS) |
| Attitude | ≤0.005° | (RMS) | |
| Position | Single point positioning: ≤1.2m(RMS) | ||
| RTK:≤2cm+1ppm(RMS) | |||
| Velocity | ≤0.02m/s | (RMS) | |
| Inertia/ODO/DVL integrated accuracy | ≤0.5%×D(D is the mileage, depending on the DVL accuracy) | ||
| Main device indicators | |||
| Gyroscope | Range | ±300 | °/s |
| Bias stability | ≤0.01 | °/h(GJB,1σ) | |
| Accelerometer | Range | ±30 | g |
| Bias stability | ≤20 | μg(GJB,1σ) | |
| Physical property | |||
| Voltage | 28V | Power consumption | ≤35W |
| Working temperature | -40ºC~+60ºC | IP grade | IP65 |
| Dimension | 190×190×166mm | Net weight | ≤7kg |
| Vibration | Meet the vibration requirements of GJB150.16A-2009 and propeller aircraft equipment | ||
| Shock | 30g,11ms, half sine | ||
| Interface Characteristics | |||
| Interface type | Channel 1: RS232; Channel 4: RS422; Channel 1: CAN;Channel 1: Ethernet; Channel 1: USB | ||
| Data update rate | Integrated navigation data: 1~800Hz (adjustable); GNSS data: 1-5 Hz | ||
| Transmission speed | 9600~921600bps (configurable) | ||
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