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Navigation and piloting system "KARAT-PNK"
It is intended for the spatial motion of an unmanned aerial vehicle in autonomous mode or by commands from an external control source, as well as for issuing navigation data for a target load.
Part number:
Description
Specifications
measurement of angles of roll, pitch accuracy up to 0.3o
course angle measurement accuracy up to 1.0
measurement of angular velocities along three axes up to ± 180o / s
measurement of linear accelerations in three axes up to ± 10m / s2
measurement of spatial coordinates accuracy up to 6m
possibility of entering differential corrections
satellite navigation receiver height measurement from -500 to 5000 m accuracy up to 10 m
measurement of airspeed up to 220 km / h accuracy up to 10 km / h
telemetry frequency up to 1 kHz
operating temperature range from -40 to +55 ° C
RS-232, RS-485, CAN interfaces
formation of PWM for control of 6-channel servo drives (6 V)
input signals from an external control unit 6 channels (6 V)
supply voltage 9-36 V
power consumption 5 W
body dimensions 115 × 70 × 24 mm
weight (housing design) 200 g
measurement of angles of roll, pitch accuracy up to 0.3o
course angle measurement accuracy up to 1.0
measurement of angular velocities along three axes up to ± 180o / s
measurement of linear accelerations in three axes up to ± 10m / s2
measurement of spatial coordinates accuracy up to 6m
possibility of entering differential corrections
satellite navigation receiver height measurement from -500 to 5000 m accuracy up to 10 m
measurement of airspeed up to 220 km / h accuracy up to 10 km / h
telemetry frequency up to 1 kHz
operating temperature range from -40 to +55 ° C
RS-232, RS-485, CAN interfaces
formation of PWM for control of 6-channel servo drives (6 V)
input signals from an external control unit 6 channels (6 V)
supply voltage 9-36 V
power consumption 5 W
body dimensions 115 × 70 × 24 mm
weight (housing design) 200 g