| 惯性导航系统仿真试验研究 |
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| 引用本文： | 王海青.惯性导航系统仿真试验研究[J].飞机设计,2007,27(5):43-48. |
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| 作者姓名： | 王海青 |
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| 作者单位： | 沈阳飞机设计研究所,辽宁,沈阳,110035;哈尔滨理工大学,计算机科学与技术学院,黑龙江,哈尔滨,150080 |
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| 摘 要： | 惯性导航系统是通过测量加速度自动推算飞机速度和位置数据的自主式导航设备,其作用是保证飞机按预定的航线飞行,准确地抵达目的地。在航空电子设备试验中,采用惯导仿真器可以减少测试的复杂性,而且还能获得更好的动态效果。本文介绍了惯导系统功能控制逻辑和显示画面的验证方法,同时还介绍了仿真器的软件编制技术。
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| 关 键 词： | 惯性导航系统 结构特点 软件设计 |
| 文章编号： | 1673-4599（2007）05-0043-06 |
| 收稿时间： | 2006-09-11 |
| 修稿时间： | 2007-07-10 |
Research of Simulation Test for Inertial Navigation System |
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| WANG Hai-qing.Research of Simulation Test for Inertial Navigation System[J].Aircraft Design,2007,27(5):43-48. |
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| Authors: | WANG Hai-qing |
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| Abstract: | Inertial navigation system is a self-contained navigation equipment which provides aircraft velocity and position data to ensure aircraft flight in a desired course to a selected destination.In the test of avionics equipment,adopting an inertial navigation simulator,complexity of test work can be reduced,and dynamic effect can be acquired better.Verification method of function control logic and displays for inertial navigation system is presented and the simulator software design technique is discussed in the paper. |
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| Keywords: | inertial navigation system structure characteristic software design |
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