摘要
为了分析变形飞行器的动态响应特性,针对后掠展长组合变形飞行器建立了动力学模型。将变形飞行器看作一个完整的多刚体系统,建立变形飞行器组合变形方程,采用多刚体理论建立了能完整描述飞行器变形过程的动力学模型。该动力学模型适用于普遍情况下的后掠展长变形飞行器。
In order to study the response characteristics of morphing aircraft,dynamic model of aircraft with sweep and span combined morphing was established. Considering a morphing aircraft which can change its wing sweep and span as a complete multi-body system,multi-body theory was used to establish the morphing aircraft＇s dynamic model. The dynamic model can be widely used in the analysis of aircraft with sweep and span combined morphing.
出处
《飞行力学》
CSCD
北大核心
2015年第5期407-410,共4页
Flight Dynamics
关键词
变形飞行器
动力学建模
多刚体系统
morphing aircraft
dynamics modeling
multi-body systems
