首页 | 本学科首页   官方微博 | 高级检索  
     检索      

两栖UAV滑跳动力学特性仿真研究
引用本文:裴譞,张宇文,王银涛,王志强.两栖UAV滑跳动力学特性仿真研究[J].计算力学学报,2011,28(2):173-177.
作者姓名:裴譞  张宇文  王银涛  王志强
作者单位:1. 西北工业大学航海学院,西安,710072
2. 昆明精密机械研究所,昆明,650118
基金项目:中国国家自然科学基金(50976017);国家自然科学基金委员会重点(50736001)资助支持.
摘    要:基于空气动力学、势流理论和二元平面滑行理论,建立了两栖UAV入水滑跳动力学模型,重点对两栖UAV入水滑跳动力学特性进行了分析,并研究了多种入水条件对滑跳状态的影响.结果显示:(1)两栖UAV触水瞬间,姿态出现明显变化,UAV出现瞬时剧烈抬头趋势;(2)两栖UAV入水攻角增大,会造成UAV较大的沾湿深度和较短的滑水时间;...

关 键 词:两栖UAV  动力学建模  滑跳状态特性  仿真分析
收稿时间:2009/4/29 0:00:00
修稿时间:2009/12/11 0:00:00

Simulation and analysis of slide jump dynamic characteristic of the amphibious UAV
PEI Xuan,ZHANG Yu-wen,WANG Yin-tao and WANG Zhi-qiang.Simulation and analysis of slide jump dynamic characteristic of the amphibious UAV[J].Chinese Journal of Computational Mechanics,2011,28(2):173-177.
Authors:PEI Xuan  ZHANG Yu-wen  WANG Yin-tao and WANG Zhi-qiang
Abstract:Based on the aerodynamic,the potential flow theory and the planning theory, a dynamic model of the slide jump ballistics of the amphibious UAV was developed. The slide jump dynamics characteristic of amphibious UAV had been analyzed in details, and the slide jump state had been researched on the impact of the several jumping condition. Results show that:(1)At the moment of touching water, posture of amphibious UAV changes violently and shows a intense rising trend instantaneously;(2)The angle of attack increasing will make the bedew depth increase and the slide time decrease;(3)The pitch angle increase will make the bedew depth decrease and the slide time increase. The work can give the theoretical foundation and study tools for the conceptual design, flight control systems design and flight stability assessment of the amphibious UAV.
Keywords:amphibious UAV  dynamics model  slide jump dynamics characteristics  simulation and analysis
本文献已被 万方数据 等数据库收录!
点击此处可从《计算力学学报》浏览原始摘要信息
点击此处可从《计算力学学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号