| 某型飞机程序模拟飞行研究 |
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| 引用本文： | 郝顺义,张宗麟,柴竹琴.某型飞机程序模拟飞行研究[J].飞行力学,2000,18(3):50-53. |
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| 作者姓名： | 郝顺义 张宗麟 柴竹琴 |
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| 作者单位： | 空军工程大学工程学院,自动化控制工程系,陕西,西安,710038 |
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| 摘 要： | 在介绍了某型飞机综合操纵方式的基础上，结合该收音机倾斜角的控制规律及航向与倾斜角的关系简化式，详细给出了程序模拟航向的实现过程和数学模型。通过采集该收音机程序模拟飞行的数据，其飞行轨迹表明所给出的数学模型能够实现飞机对计划航路点的程序模拟飞行，该结论对研制导航软件具有重要的参考价值。
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| 关 键 词： | 惯性导航 模拟飞行 综合操纵 航向控制 |
| 修稿时间： | : |
Research of program simulation flight for certain type of airplane |
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| HAO Shun-yi,ZHANG Zong-lin,CHAI Zhu-qin.Research of program simulation flight for certain type of airplane[J].Flight Dynamics,2000,18(3):50-53. |
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| Authors: | HAO Shun-yi ZHANG Zong-lin CHAI Zhu-qin |
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| Abstract: | According to the principle of inertial navigation, navigation formula is evolved, after the integrate manipulate mode of certain type of airplane is introduced, the control process and mathematical models of simulation course are presented in this paper with control law of lean angle and simplification relationship of course and lean angle. According to gathered flight datum and flight orbit, it is concluded that mathematical models of simulation course are correct to realizing automatic flight among the planned route spots known as program simulation flight and can be used as a reference in studying navigation software. |
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| Keywords: | inertial navigation simulation flight integrate manipulate course control |
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