Product / Parameter GL-303
Orientation / navigation parameters
Root mean square (RMS) error of initial heading angle determination, max, ° (1) 0.036 / cos (geographic latitude)
RMS heading hold error over 1 hour of operation, max, ° (1) 0.006
RMS roll / pitch angle determination error, max, ° (1) 0.02 (in motion)
0.01 (with fixed-base correction (ZUPT))
RMS position dead-reckoning error with correction from an external speed sensor, % of travelled distance, max (2) 0.2
RMS position dead-reckoning error in autonomous (inertial) mode, km per flight hour, max (3) 1.8
Measurement range: pitch / roll, ° ±90 / ±180
Measurement range: heading, ° 0…360
Measured angular rate range: X/Y/Z, °/s ±400
Measured acceleration range: X/Y/Z (g) ±18
Resistance to environmental factors
Operating temperature (endurance), °C -40…+55
Storage temperature (strength), °C -50…+75
Vibration (endurance) (random 100 Hz–1 kHz), g rms 3.9
Shock (strength), duration: 10 ms, waveform 40
Output data
Functional readiness time, max, s 5
Fast gyrocompassing time, max, s 360
Navigation solution rate, Hz 610 (1220 on request)
Electrical parameters
Input / output interfaces RS-232/422/485, Ethernet 100 Mbit, discrete signals
Supply voltage / power consumption 18…32 V / max 20 W
Mass and dimensions
Overall dimensions (L x W x H), mm, max 325x267x234
Weight, kg, max 20
Mean time between failures (MTBF) (calculated), h 12 000
(1) Errors are specified for a pitch angle range of ±70°
(2) For ground applications
(3) For aviation applications
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+7 (495) 481-01-27 Moscow
+7 (342) 214-90-40 Perm
sales@gyrolab.ru

Moscow: Khimki, Kurkinskoye Highway, Bldg. 2
Perm: Klubnaya St., 2


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Perm: Klubnaya St., 2
Moscow: Khimki, Kurkinskoye Highway, Bldg. 2
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