The IMU will be a key component for the WLS mission, helping the lander to achieve its soft touchdown on the lunar surface. It is designed to be an accurate and reliable instrument within a minimum volume.
The target performance is to achieve a resolution better than 1ยบ in attitude estimation with a power consumption under 1W. Its minimized mass and volume will enable small satellite missions to achieve unsurpassed attitude estimation capabilities.
The GLXP presents a fantastic technology demonstration opportunity for such technology, and emxys intends to transform the IMU into a commercial product for the space market.
