SNC500A High Precision Integrated Navigation System

Обзор

SNC500A fiber integrated navigation system is based on high-precision closed-loop fiber optic gyroscope, accelerometer and high-end GNSS receiving board, through multi-sensor fusion and rotation modulation navigation solution algorithm, to provide high-precision attitude, speed and position information, to meet the requirements of high-precision measurement and control. ▶ With swinging base/moving base alignment function ▶ High precision self-north finding without external movement requirements ▶ GNSS/ odometer /DVL and other multi-information integrated navigation ▶ Long time accuracy retention without external information assistance 2. Main application areas ▶ Large UAV benchmark INERTIAL navigation ▶ Positioning orientation ▶ Underwater platform (AUV, ROV, etc.) ▶ Intelligent mining machinery The inertial measurement unit in the INERTIAL navigation system uses three high-precision fiber optic gyroscopes with orthogonal configuration to detect the angular motion of the carrier and output digital signals proportional to the angular velocity of the carrier. Three orthogonal configuration of quartz flexible accelerometer sensitive carrier line acceleration, output proportional to its current signal, the current signal through the conversion circuit into digital signal. The INERTIAL Measurement unit outputs angular velocity and acceleration information. The inertial measurement unit (IMU) is installed on the rotating mechanism and rotates with the rotating mechanism. The GNSS board receives the satellite information, solves the navigation and positioning, and sends the navigation result to the navigation computer. The navigation computer can receive the data of gyroscope, accelerometer and GNSS, calculate the system error compensation and solve the navigation, and send real-time navigation information such as speed, position and attitude through the interface circuit in a specified period.

Технические характеристики

Основные характеристики: Project Test conditions / A0 index / B0 index, Positioning accuracy GNSS valid, single point / 1.2m（RMS） / 1.2m（RMS）, GNSS valid, RTK 2cm+1ppm（RMS） / 2cm+1ppm（RMS）, Positioning hold (GNSS failure) 1.5nm/h（50%CEP）， 5nm/2h（50%CEP） / 0.8nm/h（CEP）， 3.0nm/3h（CEP）, Heading accuracy Pelf seeking north / 0.1 Sec (lati), lati is latitude (RMS), 10min / 0.06 Sec (lati), static base alignment for 5min;0.03 Sec (lati), static base alignment for 10min;Where lati is latitude (RMS), Pourse hold (GNSS failure) 0.05 /h（RMS）， 0.1 /2h（RMS） / 0.02 /h（RMS）， 0.05 /3h（RMS）, Attitude accuracy GNSS 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 optic gyroscope Measuring range / 400 /s / 400 /s, Zero bias stability 0.02 /h / 0.01 /h, Quartz flexible accelerometer Measuring range / 20g / 20g, Communication interface RS422 / 6The baud rate is 9.6kbps ~ 921.6kbps, the default is 115.2kbps, the maximum frequency is 1000Hz (original data), and the default is 200Hz, RS232 1The baud rate is 9.6kbps ~ 921.6kbps, the default is 115.2kbps, the maximum frequency is 1000Hz (original data), and the default is 200Hz, Electrical characteristics Voltage / 24～36VDC, Power waste 30W, Structural characteristics Size / 199mm 180mm 219.5mm, Weight 6.5kg / 7.5kg (non aviation) 6.5kg (aviation optional), Use environment Working temperature / -40℃~+60℃, Storage temperature -45℃~+65℃, Vibration (with damping) 5~2000Hz，6.06g, Impact (with damping) 30g，11ms, Reliability life / >15 years, Continuous working time >24h.

Технические характеристики

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