| Sign In | Join Free | My himfr.com |
|
Shenzhen Fire Power Control Technology Co., LTD
Verified Supplier
4 Years
| Sign In | Join Free | My himfr.com |
|
4 Years
| Ask Lasest Price | |
| Brand Name : | FIREPOWER |
| Model Number : | INS500 |
| Price : | 7000$ |
| Payment Terms : | L/C,T/T,Western Union |
| Supply Ability : | 500/month |
| Delivery Time : | 1 week for sample |
Product Description
INS500 fiber-optic integrated navigation system (hereinafter referred to
as "inertial navigation") is based on high-precision closed-loop
fiber-optic gyroscope, accelerometer and high-end GNSS receiving
board, and is realized through multi-sensor fusion and navigation
calculation algorithm. It provides high-precision attitude, speed,
position and other information to meet the requirements of
high-precision measurement and control. Its main application fields
include:
Reference Inertial Navigation System of Large Unmanned Moving
Carrier
Marine compass
On-board positioning and orientation
High-precision mobile measurement
High precision stable platform
Technical Parameters
Project | Test conditions | INS500A indicator | INS500B indicator |
Positioning Precision | GNSS Valid, Single Point | 1.2m(RMS) | 1.2m(RMS) |
GNSS Valid, RTK | 2cm+1ppm(RMS) | 2cm+1ppm(RMS) | |
Position hold (GNSS failure) | 1.5nm/h(50%CEP), 5nm/2h(50%CEP) | 0.8nm/h(CEP), 3.0nm/3h(CEP) | |
Heading Precision | Self-seeking north | 0.1 ° × sec (Lati), Lati is latitude (RMS), 10 min | 0.06 ° × sec (Lati), 5min alignment of stationary base; 0.03 ° × sec (Lati), 10 min alignment of stationary base; Where Lati denotes the latitude (RMS). |
Course keeping (GNSS failure) | 0.05°/h(RMS), 0.1°/2h(RMS) | 0.02°/h(RMS), 0.05°/3h(RMS) | |
Posture Precision | GNSS is valid | 0.03°(RMS) | 0.01°(RMS) |
Attitude hold (GNSS failure) | 0.02°/h(RMS), 0.06°/2h(RMS) | 0.01°/h(RMS), 0.03°/3h(RMS) | |
Speed Precision | GNSS valid, single point L1/L2 | 0.1m/s(RMS) | 0.1m/s(RMS) |
Speed hold (GNSS failure) | 2m/s/h(RMS), 5m/s/2h(RMS) | 0.8m/s/h(RMS), 3m/s/3h(RMS) | |
Optical fiber Gyroscope | Measuring range | ±400°/s | ±400°/s |
Zero bias stability | ≤0.02°/h | ≤0.01°/h | |
Quartz Flexibility Accelerate Gauge | Measuring range | ±20g | ±20g |
Zero bias stability | ≤ 50 µg (10 s average) | ≤ 20 µg (10 s average) | |
Communication interface | RS422 | Route 6 Baud rate 9.6 kbps ~ 921.6 kbps, default 115.2k bps Frequency up to 1000Hz (raw data), default 200Hz | |
RS232 | Route 1 Baud rate 9.6 kbps ~ 921.6 kbps, default 115.2k bps Frequency up to 1000Hz (raw data), default 200Hz | ||
Electrical characteristics | Voltage | 24～36VDC | |
Power consumption | ≤30W | ||
Structural characteristics | Size | 199mm×180mm×219.5mm | |
Weight | 6.5kg | ≤ 7.5kg (non-aviation) ≤ 6.5kg (optional for aviation) | |
Use environment | Operating temperature | -40℃~+60℃ | |
Storage temperature | -45℃~+65℃ | ||
Vibration (with damping) | 5~2000Hz,6.06g | ||
Shock (with shock absorption) | 30g,11ms | ||
Reliability | Life span | > 15 years | |
Continuous working time | >24h | ||
Outline Drawing
|
|
