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High-Precision Dual-Axis Rate Table with ±3″ Accuracy and Wide Dynamic Range Redefines INS Calibration and Spacecraft Attitude Testing

Combining ±3″ accuracy, 0.0001°/s resolution, and ±0.001–350°/s range, the BE-INS2-24B21 dual-axis rate table delivers calibration for INS and spacecraft attitude systems. Designed for satellite, flight, and aerospace sensor validation, it enables characterization from low-speed drift to high-dynamic response with stability across the full range, supporting demanding R&D and production.
Jul 27th,2026 4 Views
【Wuhan, July 27, 2026】 —— As satellite constellations expand and spacecraft missions grow increasingly complex, the calibration of inertial navigation systems and attitude control components has become a critical enabler of mission success. The ability to characterize sensor performance—from barely perceptible drift to rapid dynamic response—demands test equipment that combines extreme precision with exceptional versatility. Today, we are proud to announce a new application paradigm for the BE-INS2-24B21 high-precision dual-axis rate table — not merely a positioning turntable, but a comprehensive inertial sensor validation platform tailored for INS calibration, spacecraft attitude testing, and aerospace sensor qualification.


From Arc-Minute to Arc-Second: The Precision Imperative in Inertial Testing

Conventional rate tables often struggle to deliver the combination of arc-second accuracy and fine rate resolution required for modern inertial sensors—where even minor calibration errors can propagate into significant navigation drift over extended missions. The BE-INS2-24B21 delivers ±3″ angular positioning accuracy with ±3″ repeatability and 0.36″ angular position measurement resolution, enabling precise gyroscope and accelerometer characterization. Rather than a simple positioning device, this system generates a dedicated calibration signature for each sensor under test, providing high-fidelity data for navigation system optimization and quality assurance.

Wide Dynamic Range for Comprehensive Sensor Characterization

The BE-INS2-24B21 features a broad rate range from ±0.001°/s to ±350°/s with 0.0001°/s rate resolution, supporting comprehensive characterization of gyroscope bias, scale-factor linearity, and rate response across the full operational spectrum. The system's exceptional rate stability—maintained across the entire speed range—ensures consistent, repeatable test conditions essential for reliable sensor validation. This capability is particularly critical for spacecraft attitude control systems, where sensor performance must be verified from station-keeping precision to rapid attitude maneuvers.

Sub-Arcsecond Measurement for High-Integrity Sensor Validation

The BE-INS2-24B21 achieves sub-arcsecond angular measurement capability, enabling detection of subtle sensor characteristics that might otherwise remain hidden in conventional test setups. This precision is indispensable for validating FOGs (fiber optic gyroscopes), MEMS-IMUs, and accelerometers used in satellite navigation, autonomous driving, and aerospace guidance applications. The system's high repeatability ensures that calibration results reflect only the sensor's intrinsic behavior—not equipment variation—providing engineers with data they can trust for critical design decisions.

Enabling Automated Calibration Pipelines for Production Efficiency

In response to the growing demand for operational efficiency in sensor manufacturing and validation, the BE-INS2-24B21 offers comprehensive remote control interfaces, seamlessly integrating into existing automated test frameworks. Whether for high-volume INS sensor screening or R&D-grade spacecraft component characterization, the system executes unattended calibration sequences via script-driven automation. This transition elevates inertial sensor calibration from manual craftsmanship to a data-driven, auditable, and fully traceable quality foundation—empowering aerospace manufacturers and navigation system developers with quantifiable confidence in their components.

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