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基于DSP的双发无人靶机飞控系统设计
引用本文:路引,王道波,徐扬,陈睿璟.基于DSP的双发无人靶机飞控系统设计[J].四川兵工学报,2011,32(12):42-45.
作者姓名:路引  王道波  徐扬  陈睿璟
作者单位:南京航空航天大学自动化学院,南京,210016
摘    要:针对某型无人靶机飞控系统在性能、成本、功耗以及集成度等方面的较高要求,为了适应高原打靶实验,设计了一种基于TMS320F28335的双发飞控系统。结合CCSv4.1.1软件开发平台,详细阐述了飞控系统的设计思想及软硬件结构和控制策略。半实物仿真试验表明:该双发飞行控制系统结构设计合理并满足飞行要求,具有一定的工程应用价值。

关 键 词:双发无人靶机  DSP微处理器  飞行控制系统

Design of Flight Control System Based on DSP for Double Engines Unmanned Target Drone
Authors:LU Yin  WANG Dao-bo  XU Yang  CHEN Rui-
Affiliation:jing(College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China)
Abstract:A flight control system of unmanned target drone has many requirements,such as performance,cost,power,integration,etc.In order to adapt to plateau targeting experiment,this paper presents a double engines flight control system based on TMS320F28335 microprocessor.The design scheme,hardware and software structure and strategy are expatiated in detail combined with CCSv4.1.1.1 Software development platform.The results of hardware-in-loop simulation show that the structure designed for the double engines flight control system is reasonable,and satisfies the requirements of flight quality and further engineering applications.
Keywords:double engines unmanned target drone  DSP Microprocessor  flight control system
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