The light and compact universal laser strapdown inertial satellite integrated navigation system consists of three single-axis modular digital laser gyros and a three-axis integrated photoelectric accelerometer. The system is equipped with inertial/satellite (multi-mode) deep integrated navigation, visual situation calibration prompt and automatic calibration, high-precision pure inertial low-delay output, multi-sensor navigation information fusion and other functions. It can be applied to all kinds of flight platforms.
Main performance index
Position accuracy: 0.6 nmile/h
Velocity error: 0.6m /s
Attitude accuracy: 0.05°
Weight: ≤ 6.5kg