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某型号雷达导引头测试控制系统的设计
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摘要
随着航空航天事业的发展,导弹在各国的国防建设和战略规划上占据越来越重要的地位。以美国为首的多国部队在海湾战争中实施外科手术式打击取得的辉煌战果,以及导弹在伊拉克和前南斯拉夫维和行动中的重要作用都证实了这一点。因此,导弹技术在世界范围内引起了广泛的重视。
     导弹的制导性能直接影响导弹的命中率,而导弹的制导性能是由导弹上的导引头控制的。导引头根据制导方式可以分为红外导引头,激光导引头,雷达导引头等等。由于红外、激光、可见光等在大气中传播损耗比微波波段大很多,实现距离也比较近,就使得雷达导引头成为导引头的主流发展方向。雷达导引头是武器装备和导弹发展中的关键部分,其性能直接决定导弹的制导性能。因此,在雷达导引头装上导弹之前对其进行性能测试对于保证导弹正常工作是十分重要的。近年来,各国为了在战争中立于不败之地,加紧了对雷达导引头的研究,随着国内外各种雷达导引头型号的发展,对其性能测试的要求也越来越高,课题就国内某型号雷达导引头的测试控制系统进行了设计研究。
     论文首先介绍了国内外现有的雷达导引头的发展及雷达导引头测试控制系统的发展,详尽分析了雷达导引头自动测试控制系统的主要组成和主要功能,并根据实际情况,通过某型号雷达导引头测试控制系统提出的测试技术要求和测试目的,提出了相应的设计思想和实现方案。
     测试控制系统分为目标模拟器、程控信号源和测试控制台三个部分。论文介绍了测试控制台、目标模拟器的硬件设计。并且详细介绍了目标模拟器控制器部分的工作原理和设计方法,它是由单片机和可编程逻辑控制器件共同完成的,分析了单片机和可编程逻辑控制器的工作流程。
     基于虚拟仪器技术完成了测试控制平台软件设计。通过它完成对目标模拟器,程控信号源,雷达导引头之间的数据和指令的传递,并且将测试结果显示和存储在以工业控制计算机为核心的测试控制台上。
     最后对某型号雷达导引头测试控制系统进行了试验,验证了测试控制系统的测试性能,积累了雷达导引头测控方面的相关经验,为其它型号雷达导引头测试控制系统的设计和通用型雷达导引头测试控制系统的研制打下了理论和试验基础。
Basing on the great development of aerospace technology, guided missile weapon has become more and more important to the national defence and strategic, for every country. The guided missile weapon has been proved clearly to be powerful, in the Gulf-War to Iraq and the socalled Peace-Keeping Activities in former Yugoslavia, which were both launched by USA. After that, the research and development to guided missile became blooming around the world.
     The hit successful rate of a guided missile depends directly upon the performance of its guidance system, and the later is decided by the seeker in the missile. According to the guidance way, the seeker can be classified as infrared seeker, laser seeker, radar seeker and so on. Because the propagation loss of infrared, laser and visible light are much higher than that of microwave in atmosphere, and then can only reach shorter distance than radar, that makes the microwave radar seeker became the main trend gradually. Radar seeker is the key component in missile weapons, and determines directly the guidance performance of missile. It's ncecessary and important to test the seeker completely, before installed into missile. Therefore, the development of kinds of radar seeker requires higher testing technich. In this paper, a testing and controlling system of some radar seeker is researched and designed.
     The paper introduces firstly the development of radar seeker and its testing controlling system, and describes the main parts and their function of radar seeker automation testing controlling system. And basing on the testing technical specification and testing target required by a radar seeker automation testing and controlling system, the paper bring forward the design thought and realize scheme.
     The testing and controlling system is composed by target simulator controlling, programed signal source controlling and testing & controlling platform. The paper introduces the hardware design of the testing & controlling platform and target simulator, and explain the operation principle and design method of target simulator. The target simulator is constructed with SCM and PLC. The paper analyses the work flow of SCM and PLC
     The software design of the testing control platform is based on the virtual instrument technich. It transfers the data and instruction among the target simulator, programed signal source and radar seeker. The test result is dispayed and also saved into the testing & controlling platform.
     Finally, we made a series experiments on the testing & controlling system, and verify the measurement performance of the testing & controlling platform. It accumulates experience about the radar seeker testing and controlling and prepares the theory and test foundation for the testing and controlling system of other type radar seeker and general purpose radar seeker.
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