NAV500 Inertial Navigation System (INS) | Dual-antenna directional navigation unit

15900.00 $

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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

 

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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 โ‰ค12W
Physical Size Dimensions 80×80.5x69mm
Weight โ‰ค560g
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

 

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