作者: Yu-Hui Dong , He-Shan Liu , Zi-Ren Luo , Yu-Qiong Li , Gang Jin
DOI: 10.1063/1.4891037
关键词: Noise (radio) 、 Astronomical interferometer 、 Laser beam quality 、 Adaptive optics 、 Jitter 、 Optics 、 Physics 、 Laser 、 Beam (structure) 、 Interferometry
摘要: In space laser interferometer gravitational wave (G.W.) detection missions, the stability of beam pointing direction has to be kept at 10 nrad/√Hz. Otherwise, jitter noise will dominate budget and make G.W. impossible. Disturbed by residue non-conservative forces, fluctuation could a few μrad/√Hz frequencies from 0.1 mHz Hz. Therefore, control system is an essential requirement for those missions. An on-ground test such performed, where Differential Wave-front Sensing technique used sense beams jitter. active controlled steering mirror employed adjust compensate The experimental result shows that can very large dynamic range up 5 μrad. At interested between 1 Hz, 6 nrad/√Hz achieved.