HRG-Based Inclinometer
Inclinometer
High-precision three-axis inclinometer based on hemispherical resonator gyroscopes (HRG), designed for attitude determination and integration into advanced navigation systems.
Space Heritage
Yubileiny Satellite
The three-axis inclinometer developed by MEDICON was installed onboard the Yubileiny satellite as part of its attitude determination system.
Successful operation in space confirmed the reliability of the design, resistance to environmental influences, and long-term stability of performance characteristics.
Typical Specifications
Measurement Time
120 s
Bias Stability
0.2 °/h
Noise (3σ)
< 3″
Maximum Angular Rate
±3 °/с
Power Consumption
4 Вт
Startup Time
< 30 с
Operating Temperature
−30...+80 °C
Vibration Resistance
20 g
Interface
RS-485
* Specifications correspond to one of the implemented product configurations.
Dimensions
Ø37 × 572.5 мм
Product weight — 1.4 kg
Applications
Spacecraft
Aircraft Systems
Navigation Systems
Attitude Control Systems
Special-Purpose Equipment
Scientific Instruments