海军航空工程学院学报2017，Vol.32Issue(5)：421-425,5.DOI:10.7682/j.issn.1673-1522.2017.05.001
飞翼布局无人机着舰飞行动力学分析
Analysis of the Flight Dynamic During Flying Wing UAV Carrier Landing
摘要
Abstract
Flying wing UAV has distinct aerodynamic characteristic.It's of great significance to research the flight dynam?ic character for the design of control law during the carrier-landing of flying wing UAV.A six-degree-of-freedom flight dynamic model of flying wing UAV carrier landing was presented.Based on the analysis of the flight stability of the UAV gliding,the range of approaching velocity achieving flight quality of first-class level was calculated,according to the re?quirement of the flight quality to the flight stability.Through the trim calculation and small perturbation linearization,the linear model of UAV gliding motion was obtained. The longitudinal and lateral-directional modal properties were ana?lyzed. Results showed that during the flying wing UAV gliding, the longitudinal long-periodic and short-periodic mode and the lateral-directional roll and spiral mode became convergent slowly,but the dutch roll mode was divergent.关键词
飞翼布局/着舰/飞行品质/模态特性Key words
flying-wing configuration/carrier landing/flight quality/modal properties分类
航空航天引用本文复制引用
韩维,陈志刚,张勇,阎永举..飞翼布局无人机着舰飞行动力学分析[J].海军航空工程学院学报,2017,32(5):421-425,5.基金项目
国家自然科学基金资助项目(51375490) （51375490）
