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Product Details:
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| Position: | 0.8nmile/h Inertial | Velocity: | 0.8m/s Inertial |
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| Roll & Pitch: | 0.05 ° Inertial | Heading: | 0.07° Inertial |
| Align Time: | 1.5 Min Fast | Angular Rate: | ±400°/s |
| Acceleration: | ±15g | Shock: | 15g@11ms, Half-sine |
| Vibration: | 0.04g²/Hz | MTBF: | 55000 Hrs |
| Highlight: | 0.8nmile/h imu inertial measuring unit,0.8nmile/h imu inertial navigation system,0.8m/s inertial navigation system |
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FG-980S inertial navigation system, in which the GNSS receiver embedded, adopts three high accuracy single-axis closed-loop miniature FOGs and quartz accelerometers. This system possesses the main features of very small size, light weight and lower power consumption, etc. It can be used as navigation system or information source for UAVs, helicopter, general aviation aircraft, etc.
FEATURES
l Provide self-contained, abundant, continuous and accurate navigation information
l Small size, light weight and low power consumption
l Embedded satellite navigation technology
APPLICATION
UAVs,helicopter,general aviation aircraft,etc.
STRUCTURAL DIMENSION
SPECIFICATIONS
| Alignment Time | GC: 5 min Fast: 1.5min |
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| Accuracy | Position | Inertial: 0.8nmile/h Integrated: 30m |
| Velocity | Inertial: 0.8m/s Integrated: 0.5m/s |
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| Attitude | Inertial:0.05° Integrated:0.04° |
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| Heading | Inertial: 0.07° Integrated: 0.06° |
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| Dynamic Range | Angular Rate | ±400°/s |
| Acceleration | ±15g | |
| Operation Requirement | Temperature | Work:-45~+70℃ Storage:-55~+85℃ |
| Shock | Half-sinusoid:15g,11ms | |
| Vibration | 0.04g²/HZ | |
| MTBF | 55000h | |
| Power Supply/Consumption | 28V DC/30W | |
| Interface | MIL-STD-1553B ARINC-429 RS-422 |
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| Dimension | Navigation unit: 238mm×188mm×190mm Max size: 254mm×188mm×190mm |
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| Weight | 7.1kg(excluding receiving antenna) | |
Contact Person: Yu.Jing
Tel: +8613045000776
Fax: 86-532-68977475
