发明名称 DESIGN OF A FREE-SPACE OPTICAL COMMUNICATION MODULE FOR SMALL SATELLITES
摘要 Communication bottlenecks, particularly in the downlink direction, are a common problem for many CubeSat developers. As described herein, a CubeSat module for a CubeSat comprises an optical transmitter to transmit data to a remote terminal, a receiver to acquire an optical beacon from a remote terminal, and a fine-pointing module operably and directly coupleable to a coarse-pointing module of the CubeSat. The fine-pointing module is configured to point the optical transmitter toward the remote terminal with an accuracy range that overlaps with an accuracy range of the coarse-pointing module of the CubeSat so as to establish a communications link between the CubeSat and the remote terminal over a low-Earth-orbit (LEO) distance.
申请公布号 US2016043800(A1) 申请公布日期 2016.02.11
申请号 US201514817985 申请日期 2015.08.04
申请人 KINGSBURY Ryan Wallace;RIESING Kathleen Michelle;CAHOY Kerry Lynn;NGUYEN Tam Nguyen Thuc;CAPLAN David O. 发明人 KINGSBURY Ryan Wallace;RIESING Kathleen Michelle;CAHOY Kerry Lynn;NGUYEN Tam Nguyen Thuc;CAPLAN David O.
分类号 H04B10/118 主分类号 H04B10/118
代理机构 代理人
主权项 1. A CubeSat module for a CubeSat, the CubeSat module comprising: an optical transmitter to transmit data to a remote terminal; a receiver to acquire an optical beacon from the remote terminal; and a fine-pointing module, operably coupled to a coarse-pointing module of the CubeSat, to point the optical transmitter toward the remote terminal with an accuracy range that overlaps with an accuracy range of the coarse-pointing module of the CubeSat so as to establish a communications link between the CubeSat and the remote terminal over a low-Earth-orbit (LEO) distance.
地址 Cambridge MA US