Application 1. Flight-navigation equipment: inertial navigation system units, BINS-RT-03.
Characteristics Orthogonality calibration cross-axis error: <0.14° Gyroscope bias stability: <1°/h<br /> Noise density level: 0.0015°/s Angular rate measurement range: ±300°/s Acceleration measurement range: ±6 g Operating temperature range: –40…+100°C Supply voltage: 3.0–3.6 V May be used in safety-critical applications
Equivalent: Novotel (SBG Systems) Accessories: Inertial system sensor Status: In serial production