摘要
针对卫星搭载可动点波束天线数量的增多而带来的多副天线定位指向控制问题,文中提出了一种基于单片机和FPGA的星载定位指向控制器解决方案,介绍了控制系统硬件构成和软件实现,完成了对4副天线机构的分时控制。试验结果表明,控制精度小于0.03°,性能良好。
To the question of multi-beam antennas position as the number of the mobile beam antennas loaded by thesatellite is increased, a solution based on MCU and FPGA has been reported, which could position the antenna beam effec-tively. The control system＇s hardware structure and software realization have been introduced. The system has an intuitive ca-pability of time division driving four antennas, and the test result indicates that the error between ideal position and actualposition is less than 0.03 degree and the system performs satisfactorily.
出处
《空间电子技术》
2016年第6期14-18,共5页
Space Electronic Technology
