| 直升机六自由度仿真研究 |
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| 引用本文： | 朱宇,秦超敏,高浩.直升机六自由度仿真研究[J].飞行力学,2004,22(1):45-47,51. |
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| 作者姓名： | 朱宇 秦超敏 高浩 |
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| 作者单位： | 1. 中国飞行试验研究院,飞机所,陕西,西安,710089
2. 西北工业大学,飞机系,陕西,西安,710072 |
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| 摘 要： | 建立了直升机剐体运动的六自由度仿真模型。用试飞数据进行参数识别，建立了气动导数数据库并以此计算气动力；将仿真结果与试飞结果对比，并进行了直升机机动飞行仿真计算。结果表明：六自由度仿真模型能够得到较好的仿真结果。
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| 关 键 词： | 直升机 六自由度仿真 机动飞行 地形跟踪 |
| 文章编号： | 1002-0853(2004)01-0045-03 |
Research on Six-Degree Simulation of a Helicopter |
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| ZHU Yu,QIN Chao-min,GAO Hao.Research on Six-Degree Simulation of a Helicopter[J].Flight Dynamics,2004,22(1):45-47,51. |
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| Authors: | ZHU Yu QIN Chao-min GAO Hao |
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| Institution: | ZHU Yu~1,QIN Chao-min~1,GAO Hao~2 |
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| Abstract: | A six-degree simulation model of a helicopter is established in this paper. The aerodynamic data are calculated with derivatives that can be identified from some flight-test data. The six-degree model is compared with the result of flight-test. And some maneuver flight simulations are calculated with the six-degree model. These results show that the six-degree model is good for the flight simulation of the helicopter. |
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| Keywords: | helicopter modeling simulation maneuver flight |
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