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High Precision Inertial Navigation System JYFOG005M

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High Precision Inertial Navigation System JYFOG005M

Features

? It has the function of static north seeking and moving base north seeking, and can provide north direction reference for mission equipment without additional information assistance;

? Real-time measurement of carrier triaxial angular velocity, acceleration, attitude, velocity and position information

? System can work in pure inertial navigation mode and inertial/satellite integrated navigation mode

Technical Specifications

Azimuth measurement range

0~360

Pitch angle measurement range

±90

Roll angle measurement range

±180

Maximum angular velocity

±300/s

Maximum acceleration

±10g

North seek time

=<10min

Static north seeking accuracy

=<0.06°

Moving base seeking north precision

=<0.1°

Attitude angle alignment accuracy

=<0.06°

Pure inertial orientation maintaining accuracy

=<0.06°

Pure inertial attitude maintaining accuracy

=<0.06°

Combined navigation attitude accuracy

=<0.06°

Integrated navigation heading maintains accuracy

=<0.06°

Gyro drift

=<0.1/h

Operating temperature

-20℃~55℃

storage temperature

-50℃~70℃