Production
3-axis laser gyroscope MT-401M3-axis laser gyroscope MT-401M intends for measurement of angular rotation velocity in three perpendicular planes. |
BII-5-1 INERTIAL INFORMATION UNITThe BII-5-1 inertial information unit is supplied in a complete set with the BINS-SP-1 platformless inertial navigation system ... |
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BII-6 INTERTIAL INFORMATION UNITThe BII-6 inertial information unit is supplied in a complete set with the BIMS-T platformless small-size inertial navigation system, designed to position the aircraft |
BIMS-T PLATFORMLESS INERTIAL SMALL-SIZE SYSTEMBIMS-T is designed to position the aircraft, process and display navigation and flight data. The device is based on three KL-3 laser gyros and three AK-15 quartz accelerators. |
BINS-SP-1 PLATFORMLESS INERTIAL NAVIGATION SYSTEMBINS-SP-1 is designed to position the aircraft, process and display navigation and flight data. The device is based on three KL-3 laser gyros and three AK-15 quartz accelerators. |



