Overview
FG-980S inertial navigation system, in which the GNSS receiver embedded, adopts three high accuracy single-axis closed-loop miniature FOGs and quartz accelerometers. This system possesses the main features of very small size, light weight and lower power consumption, etc. It can be used as navigation system or information source for UAVs, helicopter, general aviation aircraft, etc.
FEATURES
Provide self-contained, abundant, continuous and accurate navigation information
Small size, light weight and low power consumption
Embedded satellite navigation technology
APPLICATION
UAVs,helicopter,general aviation aircraft,etc.
STRUCTURAL DIMENSION
SPECIFICATIONS
Alignment Time GC:5min
Fast:1.5min
Accuracy Position Inertial:0.8nmile/h
Integrated:30m
Velocity Inertial:0.8m/s
Integrated:0.5m/s
Attitude Inertial:0.05°
Integrated:0.04°
Heading Inertial:0.07°
Integrated:0.06°
Dynamic Range Angular Rate ±400°/s
Acceleration ±15g
Operation Requirement Temperature Work:－45～＋70℃
Storage:－55～＋85℃
Shock Half-sinusoid:15g,11ms
Vibration 0.04g2/Hz
MTBF 50000h
Power Supply/Consumption 28VDC/30W
Interface MIL-STD-1553B
ARINC-429
RS-422
Dimension Navigation unit:238mm×188mm×190mm
Max size:254mm×188mm×190mm
Weight 7.1kg(excluding receiving antenna)