| 副翼-方向舵交联系统和稳定轴偏航阻尼器对某机抗偏离/尾旋效果研究 |
| |
| 引用本文： | 刘博强,方振平.副翼-方向舵交联系统和稳定轴偏航阻尼器对某机抗偏离/尾旋效果研究[J].飞行力学,1991(2). |
| |
| 作者姓名： | 刘博强 方振平 |
| |
| 作者单位： | 北京航空航天大学，北京航空航天大学 |
| |
| 摘 要： | 本文是在对某机尾旋特性研究的基础上,探讨引入副翼-方向舵交联系统和稳定轴偏航阻尼器对该机尾旋进入特性的影响,看其抗偏离/尾旋效果.研究方法仍采用微分方程的分支突变理论,结合时域动态响应,计算装有这类控制系统后的飞机平衡面等.
|
| 关 键 词： | 副翼-方向舵交联系统 稳定轴偏航阻尼器 偏离 尾旋 |
THE STUDY OF THE EFFECTIVENESS OF ARI AND STABILITY AXIS YAW DAMPER ON DEPARTURE/SPIN RESISTANCE FOR AN AIRCRAFT |
| |
| Liu Buoqiang,Fang Zhenping.THE STUDY OF THE EFFECTIVENESS OF ARI AND STABILITY AXIS YAW DAMPER ON DEPARTURE/SPIN RESISTANCE FOR AN AIRCRAFT[J].Flight Dynamics,1991(2). |
| |
| Authors: | Liu Buoqiang Fang Zhenping |
| |
| Institution: | Beijing University of Aeronautics and Astronautics |
| |
| Abstract: | In the paper, the effects of Aileron-Rudder-Interconnect (ARI) and stability-axis yaw damper on spin behavior are explored by the Bifurcation Analysis and Catastrophe Theory Method (BACTM) combining with the check of time history for an aircraft. The results show that the systems are effective in preventing the departure/spin of the aircraft. |
| |
| Keywords: | aileron-rudder-interconnect stability-axis yaw damper departure spin |
| 本文献已被 CNKI 等数据库收录！ |
