基于DSP的双发无人靶机飞控系统设计 |
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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. |
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作者姓名: | 路引 王道波 徐扬 陈睿璟 |
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作者单位: | 南京航空航天大学自动化学院,南京,210016 |
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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。
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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 |
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Authors: | LU Yin WANG Dao-bo XU Yang CHEN Rui- |
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Affiliation: | jing(College of Automation Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China) |
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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. |
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Keywords: | double engines unmanned target drone DSP Microprocessor flight control system |
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