某型高速无人靶机飞行控制的设计与实现  

Design and Implementation of Flight Control for High-speed Unmanned Target Drone

作　　者：郭继凯 王道波[1] 李晓萌 杨华 王博航 GUO Jikai;WANG Daobo;LI Xiaomeng;YANG Hua;WANG Bohang(College of Automation Engineering,Nanjing University of Aeronautics ancl Astronautics,Nanjing 210016,China)

机构地区：[1]南京航空航天大学自动化学院,江苏南京210016

出　　处：《机械与电子》2018年第6期54-57,61,共5页Machinery & Electronics

摘　　要：按照某型高速无人靶机飞行特性和性能要求,详细给出了以DSP为处理核心的飞行控制系统硬件组成和逻辑功能结构,介绍了无人靶机飞行控制策略,设计并开发了配套的地面测控程序,并进行靶机的半物理仿真实验。仿真结果表明,该飞行控制系统性能良好,符合高速无人靶机的飞行要求,并成功应用于某型无人机飞行试验。According to the flight characteristics and performance requirements of a high-speed unmanned target drone,this paper presents in detail the hardware composition and logic function structure of the flight control system with DSP as the processing core and introduces the flight control strategy for unmanned drone as well as the supporting ground monitoring and control procedures.A semi-physical simulation experiments of the drone has been conducted.The simulation results show that the flight control system has performed well enough to meet the flight requirements of the high-speed unmanned target drone and has been successfully applied to a drone flight test.

关 键 词：高速无人靶机 飞行控制系统 DSP微处理器 半物理仿真 

分 类 号：V279.1[航空宇航科学与技术—飞行器设计]