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作 者:张驰[1] 梁彦[2] 王天辉[1] ZHANG Chi;LIANG Yan;WANG Tianhui(91851th Unit of PLA,Huludao 125001,China;92941th Unit of PLA,Huludao 125001,China)
机构地区:[1]中国人民解放军91851部队,辽宁葫芦岛125001 [2]中国人民解放军92941部队,辽宁葫芦岛125001
出 处:《计算机测量与控制》2024年第9期177-183,共7页Computer Measurement &Control
摘 要:针对某飞行器传统发射控制装置结构复杂、操控繁琐、可靠性差的现实问题,开展便携式简易发射控制装置总体技术方案设计,基于虚拟仪器技术、构建PXI总线测控平台,采用便携式加固机箱构架、实施功能结构整合;围绕该飞行器射前性能检查和发射控制过程安全可靠要求,开展系统软硬件技术研发,完成硬件设备选型、功能结构设计与电气适配调理,实施射检发控软件功能规划与流程设计。实际使用表明:该发射控制装置结构简明优化、操控安全可靠、保障便捷高效,满足实战化发射要求。Aimed at the problems of complex structure,complicated control,and low reliability of traditional aircraft launching control devices,a general technical design for portable and simple launching control devices is carried out.This paper constructs the measurement and control platform based on Virtual Instrument and PXI bus technology,adopts the portable strengthening chassis frame to integrate the functional structure,conducts the technical development of the system software and hardware according to the requirements of safety and reliability in the pre-launch inspection and launch control process,achieves the selection of hardware equipment,design of function structure,and adjustment of electrical adaptation,and implements the function planning and process design of the pre-launch inspection and launch control software.Practical applications show that the launch control device has advantages of the simple and optimized structure,safe and reliable operation,convenient and efficient support,and the device meets the requirements of practical launch.
关 键 词:某飞行器 发射控制 PXI总线 电气适配 射前检查
分 类 号:TP241.2[自动化与计算机技术—检测技术与自动化装置]
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