飞机纵向振荡的试飞研究  

Flight Test Research of Aircraft Longitudinal Oscillation

作　　者：吕玉虎[1] 范晓明[1] 冯瑞娜[1] 

机构地区：[1]中国飞行试验研究院飞机所,陕西西安710089

出　　处：《飞行力学》2004年第1期48-51,共4页Flight Dynamics

摘　　要：介绍了产生驾驶员诱发振荡(PIO)的原因,并以某飞机发生PIO为例,分析了产生PIO的机理——法向过载相位对纵向杆力的滞后接近于180°,驾驶员模态和飞机短周期模态出现了严重耦合。操纵系统时间延迟、相位滞后、质量不平衡力以及驾驶员的输入等,都会对飞机的动态特性产生影响,在飞机的设计过程中,综合考虑各方面的因素就能极大地降低产生PIO的条件和可能性。The characters and reasons of PIO are introduced. Taking an aircraft's PIO as an example, the PIO's principle (the more than 180 degs lag of the normal load behind the stick force, and the coupling of the pilot and the aircraft's short period mode) is analyzed. Many factors, including the control system delay, the phase delay, the un-equilibrium mass force, the pilot's input and so on, will influence the aircraft's dynamic response. Synthesizing these factors in the process of aircraft design will extremely reduce the factors and possibility of PIO.

关 键 词：驾驶员诱发振荡 飞机 纵向振荡 试飞 

分 类 号：V212.1[航空宇航科学与技术—航空宇航推进理论与工程]