四旋翼无人机飞控系统设计与实现

《四旋翼无人机飞控系统设计与实现》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TP273学号GS12062295UDC密级公开工程硕士学位论文四旋翼无人机飞控系统设计与实现硕士生姓名邓博文工程领域软件工程研究方向嵌入式应用技术指导教师窦强研究员龚国辉副研究员国防科学技术大学研究生院二〇一五年四月Four-rotorUAVControlSystemDesignandRealizationCandidate：DengBowenAdvisor：DouQiangAthesisSubmittedinpartialfulfillmentoftherequirementsfortheprofessionaldegreeofM

2、asterofEngineeringinSoftwareEngineeringGraduateSchoolofNationalUniversityofDefenseTechnologyChangsha，Hunan，P.R.China（April，2015）国防科学技术大学研究生院工程硕士学位论文目录摘要.........................................................................................................................

3、......iABSTRACT.....................................................................................................................ii第一章绪论..................................................................................................................31.1课题背景与意义.........

4、....................................................................................31.2旋翼无人机综述.............................................................................................31.2.1发展历史...........................................................................

5、.....................31.2.2研究现状................................................................................................51.2.3发展趋势................................................................................................61.3小型无人机应用.............................

6、................................................................71.3.1军事领域应用........................................................................................71.3.2民用领域应用........................................................................................81.4本文的工作

7、.....................................................................................................8第二章飞行平台介绍................................................................................................102.1四旋翼飞行器组成.....................................................

8、..................................102.2机架和电池.............................................