中国科学院沈阳自动化研究所机构知识库
Advanced  
SIA OpenIR  > 机器人学研究室  > 会议论文
题名: Hardware-in-the-Loop Development System for Rotary-Wing/Fixed-Wing UAVs
作者: Qi JT(齐俊桐) ; Liu, Jinda
作者部门: 机器人学研究室
会议名称: 2013 Chinese Automation Congress
会议日期: November 7-8, 2013
会议地点: Changsha, China
会议录: 2013 Chinese Automation Congress
会议录出版者: IEEE Computer Society
会议录出版地: Washington, United States
出版日期: 2013
页码: 432-437
收录类别: EI
ISBN号: 978-1-4799-0332-0
关键词: HIL development platform ; UAV ; FlightGear
摘要: In this paper, according to many kinds of hardware-in-the-loop (HIL) simulation systems, especially for the one setting controller as the hardware part, a general HIL development platform was constructed. This platform is consisted of serial input and output communication models, which can be widely used in many kinds of Unmanned Aerial Vehicle (UAV) HIL simulation systems. Changing the UAV model in Simulink and control algorithm in hardware, a new HIL simulation model will be built. This paper references a HIL simulation platform for Rotary-Wing Unmanned Aerial Vehicle (RUAV) developed by Shenyang Institute of Automation, Chinese Academy of Science, then properly modified the communication models and successfully applied them on the Fixed-Wing UAV (FUAV) HIL simulation platform. The HIL method is an effective way to construct a more realistic development platform. The system constructed in this paper not only uses the hardware equipment as the control unit, but also represents the FUAV dynamics model in the Matlab/Simulink environment. Besides, this system also brings in the FlightGear interfacing software to help testers obviously observe the flight state changes. This development pattern brings many advantages for developing the flight dynamics models and controllers of different kinds of UAVs. Results from HIL and realistic flight simulation promote the development, improvement, and realization processes of the UAV flight control algorithms and meanwhile assess the adequacy of the flight model.
产权排序: 1
内容类型: 会议论文
URI标识: http://ir.sia.cn/handle/173321/13914
Appears in Collections:机器人学研究室_会议论文

Files in This Item: Download All
File Name/ File Size Content Type Version Access License
Hardware-in-the-Loop Development System for Rotary-Wing Fixed-Wing UAVs.pdf(235KB)----开放获取View Download
Service
Recommend this item
Sava as my favorate item
Show this item's statistics
Export Endnote File
Google Scholar
Similar articles in Google Scholar
[Qi JT(齐俊桐)]'s Articles
[Liu, Jinda]'s Articles
CSDL cross search
Similar articles in CSDL Cross Search
[Qi JT(齐俊桐)]‘s Articles
[Liu, Jinda]‘s Articles
Related Copyright Policies
Null
Social Bookmarking
Add to CiteULike Add to Connotea Add to Del.icio.us Add to Digg Add to Reddit
文件名: Hardware-in-the-Loop Development System for Rotary-Wing Fixed-Wing UAVs.pdf
格式: Adobe PDF
此文件暂不支持浏览
所有评论 (0)
暂无评论
 
评注功能仅针对注册用户开放,请您登录
您对该条目有什么异议,请填写以下表单,管理员会尽快联系您。
内 容:
Email:  *
单位:
验证码:   刷新
您在IR的使用过程中有什么好的想法或者建议可以反馈给我们。
标 题:
 *
内 容:
Email:  *
验证码:   刷新

Items in IR are protected by copyright, with all rights reserved, unless otherwise indicated.

 

 

Valid XHTML 1.0!
Copyright © 2007-2016  中国科学院沈阳自动化研究所 - Feedback
Powered by CSpace