The invention provides a space
laser communication fine tracking
assembly, which adopts a two-stage closed-
loop control system to realize high-precision tracking, the first stage adopts a
light spot centroid tracking technology and adjusts a
light beam direction in real time through elements such as an FSM fast reflector and a
CMOS camera to compensate miss distance, and the second stage adopts an
optical fiber nutation coherent tracking technology to compensate miss distance. According to the
system, the micro-electromechanical
system (MEMS) mirror, the
nutation device, photoelectric detection and the like are combined, the tracking precision is further improved through
optical fiber coupling and
frequency mixing processing, the FPGA programmable processor serves as a core to process images and signals and generate control signals to drive the reflector and the
nutation device, accurate alignment of receiving and transmitting optical axes is ensured, and efficient and stable space
laser communication is achieved. According to the invention, through combination of the first-stage
light spot positioning tracking technology and the second-stage space nutation coherent tracking technology, precise control and tracking of the
light spot position in space
laser communication are realized, and the suppression bandwidth and precision of precise tracking are effectively improved.