Chamoun Jacob, Digonnet Michel J F
Opt Lett. 2017 Apr 15;42(8):1600-1603. doi: 10.1364/OL.42.001600.
A laser-driven fiber optic gyroscope (FOG) is demonstrated with an angular random walk noise of 5.5×10 deg/√h, a drift of 6.8×10 deg/h, and an inferred scale-factor stability of 0.15 ppm, making it, to the best of our knowledge, the first laser-driven FOG to satisfy the performance requirements for inertial navigation of commercial aircraft. This is achieved using Gaussian white noise phase modulation to broaden the linewidth of the source laser and to strongly suppress the narrow-linewidth optical carrier. The performance of this laser-driven FOG is shown to have better noise and only slightly higher drift than the same FOG driven by a conventional superfluorescent fiber source. This result is validated for two lasers with widely different intrinsic coherence.
展示了一种激光驱动的光纤陀螺仪(FOG),其角随机游走噪声为5.5×10 度/√小时,漂移为6.8×10 度/小时,推断的比例因子稳定性为0.15 ppm,据我们所知,这使其成为首个满足商用飞机惯性导航性能要求的激光驱动光纤陀螺仪。这是通过高斯白噪声相位调制实现的,以拓宽源激光的线宽并强烈抑制窄线宽光载波。结果表明,这种激光驱动的光纤陀螺仪的噪声性能更好,与传统超荧光光纤源驱动的相同光纤陀螺仪相比,漂移仅略高。该结果在具有广泛不同固有相干性的两台激光器上得到了验证。