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以某飞翼飞机为例,讨论了典型飞翼飞机的基本操稳特性和动态特性。并对飞翼布局飞机和常规布局飞机的主要气动导数作了对比研究,简要说明了二者在操稳特性上的不同之处及其产生的原因,为控制增稳系统的设计提供了依据。
Taking a flying-wing aircraft as an example, the basic handling characteristics and dynamic characteristics of a typical flying-wing aircraft are discussed. The main aerodynamic derivatives of flying-wing aircraft and conventional layout aircraft are contrastively studied. The difference between the two in terms of handling characteristics and their causes are briefly described, which provides the basis for the design of stabilization system.