| 基于航天测控的实时仿真系统设计 |
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| 引用本文： | 李祥明,李永刚,郭力兵,茅文浩,吴关鹏.基于航天测控的实时仿真系统设计[J].飞行器测控学报,2011(2):9-14. |
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| 作者姓名： | 李祥明 李永刚 郭力兵 茅文浩 吴关鹏 |
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| 作者单位： | 中国卫星海上测控部; |
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| 摘 要： | 航天器发射试验具有高风险性,而承担航天器测控的测控系统规模庞大、关系复杂,其测控设备、软件的正确性关系到试验成败。仿真技术的广泛应用,使设备、软件的正确性在发射任务前就可以得到充分验证,从而提高发射试验的安全性。以航天器试验任务为背景设计的实时仿真系统,在航天测量船上得到了成功应用,取得了良好的效果。
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| 关 键 词： | 航天测控 实时仿真 软件设计 |
Design of a Real-time Aerospace TT&C Simulation System |
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| LI Xiangming,LI Yonggang,GUO Libing,MAO Wenhao,WU Guanpeng.Design of a Real-time Aerospace TT&C Simulation System[J].Journal of Spacecraft TT&C Technology,2011(2):9-14. |
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| Authors: | LI Xiangming LI Yonggang GUO Libing MAO Wenhao WU Guanpeng |
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| Institution: | LI Xiangming,LI Yonggang,GUO Libing,MAO Wenhao,WU Guanpeng(China Satellite Maritime TT&C Department,Jiangyin,Jiangsu Province 214431) |
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| Abstract: | Spacecraft launches involve constant risks and launch support TT&C systems are often of large scale and high complexity.Therefore,functional reliability of the hardware and software of TT&C systems is of critical importance to the success of a spacecraft launch mission.Making good use of simulation technology,the functional reliability of the hardware and software of a system can be fully verified before missions.A real-time simulation system is designed to meet requirements of spacecraft launch missions an... |
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| Keywords: | Aerospace TT&C Real-time Simulation Software Design |
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