基于双ARM的无人直升机飞控导航系统设计

贺天鹏; 王吉东; 胡继忠; 王 松

基于双ARM的无人直升机飞控导航系统设计

1.
北京航空航天大学航空科学与工程学院,北京 100191
2. 北京航空航天大学无人驾驶飞行器设计研究所,北京 100191

详细信息

作者简介:
贺天鹏(1980-),男,四川成都人,工程师,tianpeng_he@126.com.

中图分类号: V 249
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- 被引次数: 0
出版历程
- 收稿日期: 2009-03-03
- 网络出版日期: 2010-03-31

Design of flight control and navigation systems based on two ARM for unmanned helicopter

1.
School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
2. Research Institute of Unmanned Aerial Vehicle, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 将两片基于ARM(Advanced RISC Machine)内核的微控制器应用于某型共轴式无人直升机飞控导航系统的CPU(Central Processing Unit)模块,连同电源及舵机信号处理模块、信号处理及接口模块形成一个高度集成的嵌入式飞控导航计算机,提供的8路异步串行通讯接口、8路数字信号口,与组合导航设备、信号调理设备、收发电台和姿态稳定系统与舵机等外围设备连接构成一套完整的无人直升机数字式飞控导航系统,另配置了16MB FLASH(Flash Eeprom)用于任务与飞行状态数据记录,并基于ADS(ARM Developer Suite)集成开发环境编制了系统的飞控与自主导航软件.经地面检测与调试,该系统运行情况良好.
- 无人直升机 /
- 进阶精简指令集机器 /
- 飞控导航系统
Abstract: Central processing unit(CPU) of embeded flight control and navigation systems was designed in a certain type of coaxial unmanned helicopter by two microcontrollers based on advanced RISC machine(ARM), together with power source and servo signal processing module, signal processing and interface module, to form a highly integrated embedded flight control and navigation computer. It was provided by 8-way asynchronous serial communications interfaces, 8 digital signal ports, connected with integrated navigation equipment, signal conditioning device, radio receiver and transmitter, attitude stabilization system with the steering gear, and other peripheral devices, to constitute a complete set of embeded flight control and navigation systems of coaxial unmanned helicopter, and configure another 16MB flash eeprom(FLASH) for mission and flight data storage, the flight control and autonomous navigation software of system was developed based on ARM developer suite(ADS) integrated development environment .It is proved that running state of system is good by testing and debugging in ground.
- unmanned helicopter /
- ARM(advanced RISC machine) /
- flight control and navigation systems

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参考文献(1)

[1] 郑剑,谌利,王壬林.共轴式无人驾驶直升机导航系统的设计[J].导航,2001,37 (4) : 42-50 Zheng Jian,Chen Li,Wang Renlin.Design and implementation of the navigation systems for coaxial unmanned helicopter[J].Navigation,2001,37 (4):42-50(in Chinese) [2] NXP Semiconductors.LPC2368 user manual[M].Shanghai:NXP Semiconductors,2008:3-5 [3] 邵科.基于ARM的小型无人直升机飞行控制系统设计 .杭州:浙江大学信息科学与工程学院,2008 Shao Ke.Flight control system design for small unmanned helicopters based on ARM .Hangzhou:College of Information Science and Engineering,Zhejiang University,2008(in Chinese) [4] 戴文雯.新型无人直升机飞行控制技术研究 .南京:南京航空航天大学自动化学院,2007 Dai Wenwen.Research on flight control technology of the new unmanned helicopter .Nanjing:College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,2007(in Chinese) [5] 谌利,张晓林.一种嵌入式导航系统的研究与实现[J].遥测遥控,2003,24 (3):49-52 Chen Li,Zhang Xiaolin.Investigation and actualization of embedded navigation system[J].Journal of Telemetry,Tracking,and Command,2003,24(3):49-52(in Chinese) [6] 周立功.ARM嵌入式系统应用技术笔记:基于LPC2300(上册)[M].广州:广州致远电子有限公司,2008:67-77 Zhou Ligong.Technology notes of ARM embedded system-s application:based on LPC2300(book one)[M].Guangzhou:Guangzhou Zhiyuan Electronics Co Ltd,2008:67-77(in Chinese)

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