| RSS飞机深失速仿真研究 |
| |
| 引用本文： | 周欲晓,刘昶.RSS飞机深失速仿真研究[J].飞行力学,1996,14(4):19-24. |
| |
| 作者姓名： | 周欲晓 刘昶 |
| |
| 作者单位： | 南京航空航天大学 |
| |
| 摘 要： | 参考Ｆ－１５战斗机数学模型和原始数据，通过分支分析和突变理论方法以及数值积分时间历程法的应用，估算出Ｆ－１６飞机的分支图。分析并参考飞机分支图特性，研究飞机深失速进入特性及其改出特性。
|
| 关 键 词： | 深失速 放宽静稳定性 飞行控制 仿真 战斗机 |
The Simulation Study of Deep-Stall Characteristics for RSS Airplane |
| |
| Zhou Yuxiao, Liu chang,Yin Jianghui.The Simulation Study of Deep-Stall Characteristics for RSS Airplane[J].Flight Dynamics,1996,14(4):19-24. |
| |
| Authors: | Zhou Yuxiao Liu chang Yin Jianghui |
| |
| Institution: | Nanjing University of Aeronautics and Astronautics |
| |
| Abstract: | F-16 fighter mathematical model and its primary datas are referenced in this paper, the study ways involved the application of bifurcation analysis and calastropha theroy method (BACTM) and the usage of numerical integral time histories method to evaluate F-16 bifurcation diagram. Analyzing and referring bifurcation diagram's specific property, we study airplane deep-stall entry and recovery characteristics, considering the application of control system designed according to the idea of control configured vehicle (CCV), discussions are also made on the effects of control system parameters changes to F-16 deep-stall characteristics. |
| |
| Keywords: | Deep-stall Relaxed statics stability Bifurcation and calastropha theory Simulation |
| 本文献已被 CNKI 维普 等数据库收录！ |
