| 基于伪距伪距率的双星定位系统/SINS组合导航系统的研究与仿真 |
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| 引用本文： | 张力,林雪原,蒋国锋. 基于伪距伪距率的双星定位系统/SINS组合导航系统的研究与仿真[J]. 海军航空工程学院学报, 2004, 19(6): 618-620 |
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| 作者姓名： | 张力 林雪原 蒋国锋 |
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| 作者单位： | 海军航空工程学院电子信息工程系,烟台,264001;海装驻南京地区电子设备军事代表室,南京,210013 |
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| 摘 要： | 双星定位是我国建立起来的一种区域性定位系统(GAPS)。文中介绍了双星定位的基本原理,根据其接收机的特点,论证了双星定位与惯导组合的必然性。建立了其组合的状态、观测方程,仿真结果表明了该组合方法的可行性。
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| 关 键 词： | 双星定位 捷联惯导 卡尔曼滤波 组合 高度表 |
| 修稿时间： | 2003-09-29 |
Study and Simulation on Integrated System of Pseudorange And Pseudorange-ratio Double-Star/SINS |
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| ZHANG Li,LIN Xue-yuan,JIANG Guo-feng. Study and Simulation on Integrated System of Pseudorange And Pseudorange-ratio Double-Star/SINS[J]. Journal of Naval Aeronautical Engineering Institute, 2004, 19(6): 618-620 |
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| Authors: | ZHANG Li LIN Xue-yuan JIANG Guo-feng |
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| Affiliation: | ZHANG Li LIN Xue-yuan Department of Electronic and Information Engineering,NAEI,Yantai,264001,JIANG Guo-feng Electronic Equipment Military Representatives Office of NED in Nanjing,Nanjing,210013 |
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| Abstract: | Double-star navigation is a regional global navigation system(GAPS).This paper introduces the basic principle of GAPS,according to the characteristic of the receiver,demonstrates the certainty of GAPS/SINS integration,and builds the state and system equation.The simulated results show this integrated method is practicable. |
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| Keywords: | Double-star navigation swap-down inertial Kalman Filter altimeter integration |
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