| 某微小型卫星姿轨控计算机系统的设计 |
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| 引用本文： | 盖建宁,谢华,卫新国.某微小型卫星姿轨控计算机系统的设计[J].上海航天,2003,20(3):44-47. |
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| 作者姓名： | 盖建宁 谢华 卫新国 |
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| 作者单位： | 上海航天计算机研究所,上海,200050 |
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| 摘 要： | 为实现卫星姿轨控计算机小型化，采用TI公司的数字处理器(DSP)TMS320F206芯片作为CPU，其他逻辑采用现场可编程逻辑门阵列(FPGA)实现，并以此为基础，将姿轨控系统其他有关仪器设备集成到计算机中，形成一台复合控制设备。研究表明，DsP可用于实现姿轨控计算机的小型化，以及今后复合控制系统的设计。
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| 关 键 词： | 微小型卫星 姿态控制计算机 轨道控制计算机 设计 工作原理 数字信号处理器 |
| 文章编号： | 1006-1630(2003)03-0044-04 |
| 修稿时间： | 2002年11月18 |
Design of a Small Satellite Attitude and Orbit Control Computer |
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| GAI Jian ning,XIE Hua,WEI Xin guo.Design of a Small Satellite Attitude and Orbit Control Computer[J].Aerospace Shanghai,2003,20(3):44-47. |
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| Authors: | GAI Jian ning XIE Hua WEI Xin guo |
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| Abstract: | To realize the small satellite attitude and orbit control computer (AOCC), the digital signal processor TMS320F206 chip made by TI company is served as CPU and other logical is completed by field programmable gate array (FPGA). The other equipments are integrated into this control computer to form the multi control equipment. The results of analysis and experiment are showed that the application of digital signal processor in on board computer is possible, which is able to realize AOCC and multi control system in future. |
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| Keywords: | Small and micro satellite On board computer Attitude and orbit control computer |
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