|
|||||
|
|
| 组合升力体动力学建模与仿真 | |
| 引用本文： | 姚超,张怡哲,李正强. 组合升力体动力学建模与仿真[J]. 航空计算技术, 2010, 40(2): 57-60,64 |
| 作者姓名： | 姚超 张怡哲 李正强 |
| 作者单位： | 西北工业大学,航空学院,陕西,西安,710072;西北工业大学,航空学院,陕西,西安,710072;西北工业大学,航空学院,陕西,西安,710072 |
| 摘 要： | 设计了组合升力体总体布局，提出了新的组合升力体建模思路与方法，建立了完整的组合升力体飞行动力学数值仿真模型。建模时综合考虑了主要气动力部件的建模，详细讨论了旋翼／固定翼过渡飞行模式的建模方法。根据提出的建模方法进行了组合升力体的操纵响应分析，仿真结果证明了建模理论和方法的合理性和有效性。 |
| 关 键 词： | 组合升力体 过渡飞行模式 建模 飞行动力学 |
Combination Lift Body Dynamics Modeling and Simulation |
|
| YAO Chao,ZHANG Yi-zhe,LI Zheng-qiang. Combination Lift Body Dynamics Modeling and Simulation[J]. Aeronautical Computer Technique, 2010, 40(2): 57-60,64 | |
| Authors: | YAO Chao ZHANG Yi-zhe LI Zheng-qiang |
| Affiliation: | YAO Chao, ZHANG Yi- zhe, LI Zheng- qiang ( School of Aeronautics, Northwestern Polytechnical University, Xi＇an 710072, China ) |
| Abstract: | The conceptual project for combination lift body was designed. The new method for combination lift body modeling was proposed. A mathematical model for the combination lift body dynamics simulation was developed. In the process of modeling, the models of the primary aerodynamic components of the combination lift body were considered comprehensively. The modeling methods of rotor/fixed wing transition model were discussed in detail. The response analysis were carried out according to the modeling methods. The simulation results show the rationality and validity of modeling theories and methods. |
| Keywords: | combination lift body transition flight model modeling flight dynamics |
| 本文献已被 维普 万方数据 等数据库收录！ | |