Stellar Gyro

The NewSpace stellar gyroscope uses a COTS sensor and optics resulting in a very low-cost attitude determination system that maintains accuracy during the eclipse phase. It can achieve this by using algorithms that tolerate noise and does not require a star database. It is thus far more robust against radiation damage than a standard star mapper solution would be if based on the same components.

The NewSpace stellar gyroscope can be used to propagate a spacecraft’s attitude from a known initial condition, without drift, while sufficient stars are common across frames. The image-based rotation estimates can complement a set of MEMS rate gyroscopes to maintain a high accuracy attitude estimate at low angular rates (where MEMS gyroscope drift is most severe).


• Active pixel CMOS detector
• Small size and low mass
• No baffle required
• Low power
• Simple to interface
• Immune to Moon and Earth in FoV


• High performance 3-axis rate sensor
• Full sky sensor for agile satellites


The Stellar Gyro has passed through qualification testing and is due for the first launch in 2020.

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