- Overview
- Product Description
- Main Functions
- Product Display
- Product Parameters
- Product Structure
- Main Application Fields
- Company Profile
Basic Info.
Model NO.
GI500-B0
Heading Accuracy
0.06deg
Attitude Accuracy
0.01deg
Gyro Range
400°/S
Gyro Zero Bias Stability
≤0.01°/H
Speed Accuracy
0.1m/S
Acc Range
±20g
Accelerometer Zero Bias Stability
≤ 20µg (10 S Average)
Communication Interface
RS232, RS422
Weight
6.5kg
Vibration
5~2000Hz
Power Consumption
≤30W
Operating Temperature
-40ºC~+60ºC
Transport Package
Sponge and Box
Specification
199mm*180mm*219.5mm
Trademark
AVIC
Origin
China
Production Capacity
500/Month
Product Description
Fiber Optic GNSS Integrated Inertial Navigation System for High-Precision Measurement and Control GI500-A0 (B0) fiber-optic integrated navigation system (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:
- Large UAV Reference Inertial Navigation System
- Marine compass
- Self-propelled gun orientation
- Vehicle positioning and orientation
- High-precision mobile measurement
- High precision stable platform
- The system has inertial/satellite integrated navigation mode and pure inertial mode.
- The inertial navigation system has a built-in GNSS board. When the GNSS is valid, the inertial navigation system can perform integrated navigation with the GNSS, and provide the user with navigation parameters such as the combined position, altitude, speed, attitude, heading, acceleration, and angular velocity, and output information such as the GNSS position, altitude, and speed.
- When the GNSS is invalid, it can enter the pure inertial mode (that is, GPS fusion has never been carried out after power-on, and if it loses lock again after fusion, it belongs to the integrated navigation mode). After starting, it has accurate attitude measurement function, can output the pitch and roll course, and the pure inertia can find the north statically.
Project | Test conditions | A0 indicator | B0 indicator | |
Positioning accuracy | 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 accuracy | 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). | |
Heading keeping (GNSS failure) | 0.05°/h(RMS), 0.1°/2h(RMS) | 0.02°/h(RMS), 0.05°/3h(RMS) | ||
Attitude accuracy | 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 accuracy | 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) | ||
Fiber optical Gyroscope | Measuring range | ±400°/s | ±400°/s | |
Zero bias stability | ≤0.02°/h | ≤0.01°/h | ||
Quartz flexibility Accelerometer | 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 | -40ºC~+60ºC | ||
Storage temperature | -45ºC~+65ºC | |||
Vibration with shock absorption) | 5~2000Hz,6.06g | |||
Shock (with shock absorption) | 30g,11ms | |||
Reliability | Life span | > 15 years | ||
Continuous working time | >24h |