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本文阐述了飞行器横向-航向耦合振荡形成机理,给出自动器关闭和工作时的耦合条件,分析有关气动参数及飞行状态对耦合特性的影响,讨论了飞行品质规范对横向-航向耦合模态特性的要求.
In this paper, the formation mechanism of aircraft transverse-heading coupled oscillation is described. The coupling conditions of the actuator when it is closed and working are given. The influence of aerodynamic parameters and flight conditions on the coupling characteristics is analyzed. The effects of flight quality specifications on the transverse- Request.