Design of UAV flight control ATS based on PXIbus

摘要

UAV flight control ATS based on PXIbus was designed with the application of modular instrument and virtual instrument technology for the requirements of automation,modularization and general purpose to flight control system(FCS);Signal connection platform was designed and implemented,and test software was developed used the modularization and object oriented technology under Visual C++ environment,and test interface was designed based on LabVIEW controls.The system was proved to be stable working,easily operated,and easily extended,and can improve the maintenance ability to UAV equipment of the army.Software and hardware architecture of the system,main design thought and some techniques are introduced.