Customization: | Available |
---|---|
Accuracy: | <1mm |
Horizontal Line: | 1 |
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IF3900-A | IF3900-B | Unit | ||
System accuracy | ||||
Pure inertial alignment accuracy | North finding accuracy | ≤0.01°×secφ | ≤0.015°×secφ | RMS |
Attitude accuracy | ≤0.002° | ≤0.005° | RMS | |
X`Pure inertia retention accuracy | Heading angle | ≤0.01° | ≤0.015° | RMS,1h |
Attitude angle | ≤0.002° | ≤0.005° | RMS,1h | |
Position | ≤0.2nmile/h | ≤1nmile/h | CEP50% | |
Velocity | ≤0.1m/s | ≤0.5m/s | RMS,1h | |
Inertial/satellite combination accuracy | Course | ≤0.01° | ≤0.015° | RMS |
Attitude | ≤0.002° | ≤0.005° | RMS | |
Position | Single point positioning: ≤ 1.2m,RTK: ≤ 2cm+1ppm | Single point positioning: ≤ 2m,RTK: ≤ 2cm+1ppm | RMS | |
Velocity | ≤0.02m/s | ≤0.02m/s | RMS | |
Inertia/ODO/DVL combination accuracy | Odometer/DVL combination | ≤ 0.3% × D (D is the mileage, depending on DVL accuracy) | ||
Main device indicators | ||||
Gyroscope | Range | ±500 | ±500 | °/s |
Zero bias stability | ≤0.001 | ≤0.003 | °/h(GJB, 1σ) | |
Accelerometer | Range | ±30 | ±30 | g |
Zero bias stability | ≤10 | ≤20 | μg (GJB,1σ) | |
Physical characteristics | ||||
Supply voltage | 28V | Power waste | ≤35W | |
working temperature | -40ºC~+60ºC | Protection level | IP65 | |
Physical dimensions | 190×190×166mm | Weight | ≤8.5kg | |
Vibration | Meet the vibration requirements of GJB150.16A-2009 and propeller aircraft equipment | |||
Shock | 30g, 11ms, 1/2 sine wave | |||
Interface Characteristics | ||||
Interface form | 1 RS232, 4 RS422, 1 CAN port, 1 Ethernet port, 1 USB port | |||
Data update rate | Integrated navigation data: 1~800Hz (adjustable); | |||
GNSS data: 1-5 Hz | ||||
transmission speed | 9600~921600bps (configurable) |