计算机技术与发展2017，Vol.27Issue(2)：125-129,5.DOI:10.3969/j.issn.1673-629X.2017.02.028
小型变体无人机动力学建模及配平分析
Dynamics Modeling and Trimming Analysis for Small Morphing UAV
摘要
Abstract
In order to better analyze the dynamic response of morphing Unmanned Aerial Vehicle (UAV),the moving of the center of gravity is described by quiet moment,and the six free nonlinear equations of motion for a small variable sweep UAV is derived.The kinematic equation of morphing aircraft has more items that are inertial force and inertial moment than fixed wing plane.The aerodynamicforces and moments in the process of morphing are calculated with the quasi-steady assumption,the aerodynamic force is depended on the static configuration and flight state of morphing aircraft at the moment of morphing.From the results it can be known that the main variable that affects the aerodynamic parameters ie sweep angle and angle of attack within a certain range of flight speed and altitude.To make sure that the morphing aircraft has an ideal static stability margin,the responsible position of the center of gravity on the longitudinal axis of the body at different configurations is obtained by trimming,which lays a foundation for the control system design for the morphing aircraft.关键词
变体无人机/运动方程/动态响应/配平Key words
morphing UAV/equations of motion/dynamic response/trimming分类
信息技术与安全科学引用本文复制引用
陈伟,冯高鹏,拜云山..小型变体无人机动力学建模及配平分析[J].计算机技术与发展,2017,27(2):125-129,5.基金项目
国家自然基金联合基金(U1430113) （U1430113）
中国工程物理研究院科学技术发展基金(2014B0101009) （2014B0101009）
