Paper
5 November 2015 The index analysis and structure selection of LEO space laser communication terminal
Author Affiliations +
Proceedings Volume 9795, Selected Papers of the Photoelectronic Technology Committee Conferences held June–July 2015; 97950F (2015) https://doi.org/10.1117/12.2208840
Event: Selected Proceedings of the Photoelectronic Technology Committee Conferences held June-July 2015, 2015, Hefei, Suzhou, and Harbin, China
Abstract
In order to achieve low orbit optical compartment for three generations of high-speed laser communication links which between geostationary relay satellite, It had to be designed to meet the use of laser communication terminal background paper for this with the background and the optical compartment specific installation location of the remote machine indicators such as the range of rotation, can pass the time, coarse tracking accuracy, the fundamental frequency, rotational speed, acceleration and weight were analyzed. Obtain azimuth rotation range of ± 135 °, pitching rotation range of ± 60 °, 24h passing time 50525.912s, coarse tracking accuracy 49.4 μrad other indicators, and the typical space laser communication terminal structure were analyzed according to indicators and program aims to analyze the advantages and disadvantages of the requirements proposed structure for this project, tracking frame structure is based on the optical path of the KUDE Cross.
© (2015) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
Jiaqi Zhang and Lizhong Zhang "The index analysis and structure selection of LEO space laser communication terminal", Proc. SPIE 9795, Selected Papers of the Photoelectronic Technology Committee Conferences held June–July 2015, 97950F (5 November 2015); https://doi.org/10.1117/12.2208840
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KEYWORDS
Laser communications

Mirrors

Optical communications

Optical tracking

Servomechanisms

Satellites

Satellite communications

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