摘要
针对某新型涵道无人飞行器飞行控制系统在性能、集成度等方面的较高要求,设计了一套飞行控制系统软件。提出了该飞行控制系统软件的总体设计方案,基于TASKING编程开发环境,开发了机载飞行控制软件,主要包括传感器信号采集模块、控制律解算模块、执行机构的指令信号输出模块以及无线数据通信模块;基于VC++6.0编程开发环境,开发了地面遥控遥测软件。实际飞行试验表明:该飞行控制系统软件设计合理并满足飞行要求,具有一定的工程应用价值。
The flight control system of novel ducted UAV has many requirements,such as performance,integration,etc. A software design on flight control system was designed. This paper presented the overall designable program of flight control system software in detail. Combined with TASKING Software development platform,the onboard flight control software was designed,includingsensor signal acquisition module,the control law solver module,actuator command signal output module and wireless data communication module. Based on VC ＋＋ 6. 0 programming development environment,the ground command measurement control system software was designed. The actual flight test shows that the software designed for novel ducted UAV flight control system is reasonable and satisfied with the requirements of flight quality,which has certain further evaluation in engineering applications.
出处
《四川兵工学报》
CAS
2015年第3期117-120,共4页
Journal of Sichuan Ordnance
