Fibre optic gyroscopes for space use

Nicolas Faussot, Yann Cottreau, Guillaume Hardy, Pascal Simonpietri, Thierry Gaiffe, Georges Otrio
2017 International Conference on Space Optics — ICSO 2000  
Among the technologies available for gyroscopes usable in space, the Fibre Optic Gyroscope (FOG) technology appears to be the most suitable: no moving parts, very good lifetime, low power consumption, very low random walk, arbitrarily low angular resolution and very good behaviour in radiations and vacuum. Benefiting from more than ten years of experience with this technology, Ixsea (formerly the Navigation Division of Photonetics) is developing space FOG under both CNES and ESA contracts since
more » ... ESA contracts since many years. In the 1996-1998 period, two space FOG demonstrators in the 0,01 °/h class were manufactured, including an optical head (optic and optoelectronic part) designed for space use and a standard ground electronics. Beyond the demonstration of the specified FOG performances, the behaviour of the optical head has been validated for use in typical space environment: vibrations, shocks, radiations (up to 50 krad) and thermal vacuum. Since the beginning of 1999, Ixsea is developing a space electronics in order to manufacture two complete space FOG. The first one entered in qualification in October. The second one will be delivered beginning of next year, it will be used in a CNES attitude measurement experiment (MAGI) onboard the French-Brazilian Microsatellite (FBM) partly dedicated to technology evaluation.
doi:10.1117/12.2307895 fatcat:bwalicqomvawnh6okrl2bdmjqm