翼伞动力学与动目标归航研究

《翼伞动力学与动目标归航研究》由会员上传分享，免费在线阅读，更多相关内容在学术论文-天天文库。

1、分类号V412;V525学号14010012UDC密级公开工学硕士学位论文翼伞动力学与动目标归航研究硕士生姓名周靓学科专业力学研究方向物伞多体系统动力学指导教师张青斌副教授国防科学技术大学研究生院二〇一六年十一月ResearchonDynamicsandMovingTargetHomingBasedonParachuteCandidate：ZhouLiangSupervisor：ViceProf.ZhangQinbingAdissertationSubmittedinpartialfulfillmentoftherequirementsforthedegreeofMasterofEngi

2、neeringinMechanicsDecember，2016国防科学技术大学研究生院硕士学位论文目录第一章绪论....................................................................................................................11.1研究背景和意义.............................................................................................11.2国内外研究现状..........

3、...................................................................................21.2.1静目标空投现状....................................................................................21.2.2动目标空投研究现状............................................................................41.3相关领域研究进展..............

4、...........................................................................71.3.1飞行动力学............................................................................................71.3.2翼伞航迹规划........................................................................................91.4本文研究内容.........

5、......................................................................................13第二章基于拟坐标拉格朗日法的翼伞系统建模......................................................152.1引言...............................................................................................................152.2八自由度模型......

6、.........................................................................................152.2.1建立坐标系..........................................................................................152.2.2质量矩阵计算......................................................................................172.3翼伞

7、系统气动力分析...................................................................................182.3.1纵向静稳定性分析..............................................................................182.3.2气动力计算.......................