The CFI-200 family of inertial measurement units (IMUs) offers a range of performance options tailored to meet specific requirements. These ITAR-free sensors are engineered with a focus on optimizing size, weight, power, and cost (SWaP-C), incorporating advanced closed-loop fiber optic gyroscopes and MEMS accelerometers.
Compact and lightweight, the CFI-200 IMUs provide accurate outputs of inertial linear accelerations, incremental angles, and velocities, along with status information on internal sensors and electronics. Designed for high-performance applications, they are ideal for stabilizing high-bandwidth (>1kHz) EO/IR sensors, guidance, navigation, and control (GNC) systems for space launchers, as well as integration into higher-order systems like AHRS or INS.
Specifications:
| Dimensions (D x H): | 88.9 x 93.5 mm |
| Weight: | <850g |
| Power: | 10-35VDC, 10W |
| Gyro Bias Accuracy (1σ): | < 0.85 – 0.25 °/hr |
| Gyro Max Rate: | ± 900 – 1900 °/sec |
| ARW: | < 0.018 to 0.008 °/√hr |
| Accelerometer Bias Accuracy: | 0.15 to 1 mg |
| Accelerometer Range: | ±40/60/80g |
| VRW: | < 0.04 m/sec/√hr |
