基于复杂参数的组态化显示监控系统
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摘要
随着我国航天飞行器发射频率的不断提高,以及各类预先研究型号的增多,对飞行器的测试效率提出了更高的要求;传统测发控软件由于型号需求差异,人员安排等问题,软件的设计与实现手段不同,一套软件通常只能针对一个型号,需求一旦变更,需要花费大量的人力财力开发与维护软件,同时也对保障软件的可靠性带来难度;为克服现有技术的不足,对组态化设计进行研究,采用了通用化接口设计及显示终端界面加载与数据显示方法关键技术,提出了一种基于复杂参数组态化显控系统,达到一套软件应用于多个型号的通用化目标,极大降低了控件灵活扩展与集成的难度,实现飞行器复杂参数测试数据的实时监控与软件的复用,大大提高了开发效率。
With the continuous improvement of the launching frequency of vehicles in China and the increase of various types of pre-research models,higher requirements for the testing efficiency of aircraft have been put forward.Because of the different model requirements,people arrangement problem and various design and implement methods,the traditional testing launching and control software can only used to one model.Since the requirements change,huge human recourse and money need to be cost to develop and maintain the software,and it will also bring the difficulties to the software reliability.In order to overcome existing technical deficiencies,researching the configuration design,using the key techniques of generalized interface design and display terminal loading and data displaying method,proposed a configuration display and monitor system based on complex parameters.It reached the generalized goal of one system applies to multiple models,and decreased the difficulties of the controls flexible extension and integration.The system implemented real-time monitor of the aircraft complex parameters and reuse of the system,increased development efficiency very much.
With the continuous improvement of the launching frequency of vehicles in China and the increase of various types of pre-research models,higher requirements for the testing efficiency of aircraft have been put forward.Because of the different model requirements,people arrangement problem and various design and implement methods,the traditional testing launching and control software can only used to one model.Since the requirements change,huge human recourse and money need to be cost to develop and maintain the software,and it will also bring the difficulties to the software reliability.In order to overcome existing technical deficiencies,researching the configuration design,using the key techniques of generalized interface design and display terminal loading and data displaying method,proposed a configuration display and monitor system based on complex parameters.It reached the generalized goal of one system applies to multiple models,and decreased the difficulties of the controls flexible extension and integration.The system implemented real-time monitor of the aircraft complex parameters and reuse of the system,increased development efficiency very much.
引文
[1]宋征宇.新一代航天运输系统测发控技术发展的方向[J].航天控制,2013,31(4):3-9.
[2]冀航.基于组态技术的通用运载火箭遥测数据处理平台研究与实现[D].南京:南京理工大学,2013:2-3.
[3]刘青普.面向监控的测控站仿真系统的设计与实现[J].仿真技术,2007,23:241.
[4]韩亮.测发控软件组态开发平台的设计与应用[J].计算机测量与控制,2014,23(5):1795.
[5]葛东明,黄显林.面向控制的高超声速飞行器动力学特性分析[J].航天控制,2010,28(4):3-9.
[6]程进,冯大伟,段春泉.飞航导弹变结构过载控制方案研究[J].航天控制,2008,26(2):35-40.
[7]宋征宇.新一代航天运输系统测发控技术发展的方向[J].航天控制,2013,31(4):3-4.
[8]陈涛,徐小力.基于组态王的大型烟机检测诊断系统研究[J].故障诊断,2007,23:221.
[9]曾贵明.飞行器测发控技术[M].计算机测量与控制,2009(9).
[10]王思平.测控软件通用仿真测试平台研究与实现[D].北京:北京工业大学,2015.
[11]送海涛.组态软件技术及靶场测控软件系统的设计[J].航天控制,2008,26(1):71.
[2]冀航.基于组态技术的通用运载火箭遥测数据处理平台研究与实现[D].南京:南京理工大学,2013:2-3.
[3]刘青普.面向监控的测控站仿真系统的设计与实现[J].仿真技术,2007,23:241.
[4]韩亮.测发控软件组态开发平台的设计与应用[J].计算机测量与控制,2014,23(5):1795.
[5]葛东明,黄显林.面向控制的高超声速飞行器动力学特性分析[J].航天控制,2010,28(4):3-9.
[6]程进,冯大伟,段春泉.飞航导弹变结构过载控制方案研究[J].航天控制,2008,26(2):35-40.
[7]宋征宇.新一代航天运输系统测发控技术发展的方向[J].航天控制,2013,31(4):3-4.
[8]陈涛,徐小力.基于组态王的大型烟机检测诊断系统研究[J].故障诊断,2007,23:221.
[9]曾贵明.飞行器测发控技术[M].计算机测量与控制,2009(9).
[10]王思平.测控软件通用仿真测试平台研究与实现[D].北京:北京工业大学,2015.
[11]送海涛.组态软件技术及靶场测控软件系统的设计[J].航天控制,2008,26(1):71.