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基于PC104和DSP的某型无人机导航/飞控系统设计
引用本文:贲宗玉,袁冬莉,高建尧.基于PC104和DSP的某型无人机导航/飞控系统设计[J].弹箭与制导学报,2007,27(3):23-26.
作者姓名:贲宗玉  袁冬莉  高建尧
作者单位:西北工业大学自动化学院,西安,710072
摘    要:文中介绍了一种新的基于PC104和DSP的某型无人机导航/飞控系统,给出了相应的硬件结构和软件流程.该系统采用某型PC104和 DSPF2812为核心部件,具有结构紧凑、多串口通信可靠、控制通路流畅、接口灵活等特点.最后提及了一种验证系统设计是否合理的方法,且根据试验结果证明该系统功能完善、性能可靠.

关 键 词:无人机  导航飞控系统  DSP  PC104
收稿时间:2006-08-07
修稿时间:2006-08-072006-11-13

Navigation/Flight Control System Design of Certain UAV Based on PC104 and DSP
BEN Zong-yu,YUAN Dong-li,GAO Jian-yao.Navigation/Flight Control System Design of Certain UAV Based on PC104 and DSP[J].Journal of Projectiles Rockets Missiles and Guidance,2007,27(3):23-26.
Authors:BEN Zong-yu  YUAN Dong-li  GAO Jian-yao
Abstract:In this paper, a new navigation/flight control system design of certain UAV based on PC104 and DSP is introduced. The structure of navigation/flight control system is presented as well as the software. The control system is mainly composed of PC104 and DSPF2812. The structure is compact, and multi serial communication is credible. The control access is fluent, and the interface is flexible. At the end ,one method of testing for rationality of the system design is put up. And the results are given which show the navigation and flight control system is multifunctional and reliable.
Keywords:UAV navigation/flight control system DSP PC104
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