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基于586-Engine的无人机飞控系统的设计与实现
引用本文:李昕,杨睿.基于586-Engine的无人机飞控系统的设计与实现[J].航空电子技术,2008,39(2).
作者姓名:李昕  杨睿
作者单位:南京航空航天大学自动化学院,南京,210016
摘    要:以微控制模块586-Engine为核心,设计了用于某小型无人机的一种飞行控制系统,该系统具有小型化、高集成度等特点。详细介绍了该系统的体系结构和各模块的作用,给出了相应的飞行控制策略;还介绍了飞控软件的开发环境和相应的软件流程图。半物理仿真实验表明,该无人机的飞控系统功能完善,具有较高的控制精度。

关 键 词:无人机  586-Engine微机  飞行控制系统

Design and Realization of the Flight Control System Based on 586-Engine for UAV
LI Xin,YANG Rui.Design and Realization of the Flight Control System Based on 586-Engine for UAV[J].Avionics Technology,2008,39(2).
Authors:LI Xin  YANG Rui
Abstract:A flight control system based on 586-Engine microprocessor is designed in this paper,which has many properties such as miniaturization,high-integration,etc.The structure of the control system and functional modules are introduced in detail.Also the flight control policy and relative software structure are described.The results of hardware- in-the-loop simulation indicate that the flight control system has perfect functionality and can achieve higher control precision.
Keywords:UAV  586-Engine microprocessor  flight control system  
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