| 矩形翼飞机对大气紊流的动态响应 |
| |
| 引用本文： | 叶炜樑. 矩形翼飞机对大气紊流的动态响应[J]. 南京航空航天大学学报, 1986, 0(Z1) |
| |
| 作者姓名： | 叶炜樑 |
| |
| 摘 要： | 本文采用时间历程法和谱分析技术,计算了一架典型矩形翼飞机对大气紊流的纵向动态响应,讨论了展弦比对动态响应的影响,分析了带有理想驾驶仪方程时对响应的改善。由于计算是从基本飞行运动方程出发,故对紊流的离散型和连续型有统一的求解方法。
|
| 关 键 词： | 无人驾驶飞机 飞行力学 紊流特性 动态响应 |
Dynamic Response of an Aircraft with Rectangular Wing to Atmospheric Turbulence |
| |
| Ye Weiliang. Dynamic Response of an Aircraft with Rectangular Wing to Atmospheric Turbulence[J]. Journal of Nanjing University of Aeronautics & Astronautics, 1986, 0(Z1) |
| |
| Authors: | Ye Weiliang |
| |
| Affiliation: | Ye Weiliang |
| |
| Abstract: | Adopting the-method of time course and spectral analysis technique, this paper, calculated the dynamic response of a typical rectangular wing aircraft to atmospheric turbulence. The influence of aspect ratio to dynamic response was discussed and the improving extent of dynamic response with the ideal autopilot equation was analysed.Because the response calculations are all based on the flight kinetic equations, the solutions for discrete and continuous gust models can be obtained using the similar method. |
| |
| Keywords: | pilotless. aircraft flight mechanics turbulence characteristic dynaimic response. |
| 本文献已被 CNKI 等数据库收录！ |
|
