NAV500 Inertial Navigation System (INS) | Dual-antenna directional navigation unit
15900.00 $
Description
NAV500 Inertial Navigation System (INS)
NAV500 INS is a cost-effective, compact fiber-optic inertial/satellite combined navigation system with a built-in three-axis high-precision fiber-optic gyroscope, a three-axis high-precision accelerometer, and a high-precision barometer. It integrates a full-system full-frequency GNSS dual-antenna board internally and can perform inertial/satellite combined navigation. When the GNSS information is invalid, it has a high ability to maintain pure inertial navigation accuracy.
- Application areas: aviation, UAVs, unmanned ships, vehicles, and other application scenarios.
- small size
- lightweight
- High accuracy
- Low power and high reliability
- Long life
If you have any questions regarding our products, use the Motionew Contact us page to consult our engineering team.
Specifications
Positioning Accuracy | (GNSS valid single point) | 1.2m (RMS) |
GNSS valid RTK | 1cm + 1ppm (RMS) | |
Pure inertial horizontal positioning | 100m/5min (CEP) | |
500m/10min (CEP) | ||
1.5mile/30min (CEP) | ||
Heading Accuracy | Single Antenna | 0.1ยฐ |
Dual Antenna | 0.2ยฐ/L (RMS) | |
Course Keeping | 0.2ยฐ/30min (RMS) | |
0.5ยฐ/h (RMS) | ||
Attitude Accuracy | GNSS Valid | 0.02ยฐ (RMS) |
Attitude Hold (GNSS Valid) | 0.2ยฐ/30min (RMS) | |
0.5ยฐ/h (RMS) | ||
Speed Accuracy | GNSS Valid (single point L1/L2) | 0.1m/s (RMS) |
Fiber Optic Gyroscope | Maximum Range | ยฑ500ยฐ/s |
Bias Stability | <0.2ยฐ/h | |
MEMS Accelerometer | Maximum Range | ยฑ40g |
Bias Stability | <75ฮผg | |
Electrical Characteristics | Voltage | 9~36v |
Power Consumption | โค12W | |
Physical Size | Dimensions | 80×80.5x69mm |
Weight | โค560g | |
Environmental | Working Temperature | -45ยฐC ~ +70ยฐC |
Storage Temperature | -55ยฐC ~ +80ยฐC | |
Life Span | > 15 years | |
Working hours | >24 hours | |
Interface Features | 2x RS422 (can be configured as RS232) | |
3x RS232 | ||
2x PPS |
Product contents
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Documents
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