某超低空型无人机飞控系统设计与实现  

Design and Realization of Flight Control System of Certain Type Super-Low-Altitude UAV

作　　者：姜杨[1] 王雷[1] 米阳[1] 

机构地区：[1]中国人民解放军92419部队

出　　处：《兵工自动化》2013年第10期69-70,75,共3页Ordnance Industry Automation

摘　　要：以四片微处理器为核心,研制出某超低空型无人机飞控系统。给出飞控系统总体示意图,其软件设计采用5种控制模态。探讨超低空掠海飞行的关键技术,运用半实物仿真原理,通过仿真电缆对其进行实验室仿真。仿真结果表明:该飞控系统设计是可行、正确的,能实现超低空掠海20 m飞行,系统工作正常,已被其他型号无人机飞控系统推广使用。Takes 4 microcomputers as the core, certain type super-low-altitude UAV flight control system was proposed. Put forward scheme of flight control system. Its software design adopts 5 control modes. Discuss the key technology for super-low-altitude sea skimming, use semi-object simulation principle. Use simulation cable to carry out lab simulation. The simulation results show that the flight control system design is feasible and correct. It can realize sea skimming 20 meters above the sea. The system runs smoothlv. It has used for other types UAV flight control system.

关 键 词：无人机 飞控系统 仿真 

分 类 号：TJ85[兵器科学与技术—武器系统与运用工程]