Combined navigation system
The Combined Navigation System (CNS) provides accurate measurement of coordinates and orientation of highly dynamic aircraft and vehicles.
The CNS includes an inertial measuring module, an anti-jamming four-system (GLONASS, GPS, Galileo, BeiDou) dual-frequency receiver of signals from global navigation satellite systems (GNSS) and a complex processing module.
|Maximum ground speed, m / s||1600||Data output frequency, Hz||≥100|
|Angle measurement range, degrees
||Determination error in inertial satellite mode, RMS:
|Range of variation of angular velocities, deg/s||±300||Operating temperature range, ° С||-40…+60|
|Vibration resistance (up to 2000 Hz), g||5||Reduced atmospheric pressure, Pa||100|
|Measurement range of linear acceleration,g:
||Exchange protocol, (as agreed with the consumer)||RS-485, Ethernet|
|Overall dimensions, mm||135x87x92||Weight (depends on the BChE model), kg||0.69-0.77|