The SILEX optical interorbit link experiment
暂无分享,去创建一个
The implementation of communication links between a low earth-orbiting satellite and a geostationary one, or between two geostationary satellites, will lead to significant improvements in the performance of space communication systems. Optical technology is attractive for these applications when high-data-rateCommunication is required. The European Space Agency (ESA) has therefore instigated and in-ordbit demonstration project known as SILEX (semiconductor laser intersatellite link experiment) using a pre-operational link between the French SPOT-4 low earth orbit satellite and the ESA Advanced Relay and Technology Mission Satellite(ARTEMIS). Such and optical communication system brings some new and challenging requirements. In particular, the communication beam, which has a divergence of around 6 μrad, must achieve and maintain a very demanding pointing accuracy in the presence of both host satellite vibration and relative satellite motion. This paper provides an overview of the SILEX project and describes a novel pointing mechanism.
[1] Andrew D. MacGregor,et al. A 39-photon/bit direct-detection receiver at 810 nm, BER = 1x10-6, 60-Mbit/s QPPM , 1991, Photonics West - Lasers and Applications in Science and Engineering.
[2] David J. Purll,et al. Tracking Sensor Developments For Optical Intersatellite Links , 1989, Other Conferences.