| 惯导/双星组合系统仿真系统的开发 |
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| 引用本文： | 胡珊,罗建军,袁建平.惯导/双星组合系统仿真系统的开发[J].系统仿真学报,2004,16(9):1957-1960. |
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| 作者姓名： | 胡珊 罗建军 袁建平 |
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| 作者单位： | 西北工业大学,航天学院,陕西,西安,710072 |
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| 摘 要： | 在分析惯导/双星多种不同组合模式及其数学模型的基础上,搭建仿真系统的框架结构整个仿真体系分类明确,结构合理,并根据数学模型编写了各子模块软件包,以巡航导弹的飞行实例,验证了模型的正确性和仿真软件系统具有较好的实用性。
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| 关 键 词： | 惯导系统(INS) 双星系统(DS) 卡尔曼滤波 仿真系统 |
| 文章编号： | 1004-731X(2004)09-1957-04 |
| 修稿时间： | 2003年7月2日 |
Development of Simulation System of INS/ DS Integrated System |
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| HU Shan,LUO Jian-jun,YUAN Jian-ping.Development of Simulation System of INS/ DS Integrated System[J].Journal of System Simulation,2004,16(9):1957-1960. |
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| Authors: | HU Shan LUO Jian-jun YUAN Jian-ping |
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| Abstract: | Different patterns of INS/DS (Double Satellite) integrated navigation system and their mathematical models are analyzed synthetically in this paper. Based on them, the simulation system is constructed. The software of each sub-model is programmed. The whole simulation system is classified clearly and the frame of the system is logical. An example of cruise missile is given to verify the efficiency and practicability of the simulation system. |
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| Keywords: | inertial navigation system (INS) double satellite (DS) Kalman filter simulation system |
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