近程反导火箭炮发射结构研究
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摘要
随着世界军事技术的飞速发展,火箭武器被赋予了新的历史使命即应用于防空作战。本文在对现有近程反导自动火箭炮的作战需求分析和装备需求分析的基础上,提出了火箭炮的总体概念。详细的分析了几个子系统的功能、结构、性能,并对几个子系统进行了设计。
本文将模拟和数字电子技术、数据通信、控制技术、单片机技术综合应用于火箭炮点火控制系统的设计,通过对控制系统的结构、构成及应用的深入研究,成功的设计了适用不同管数的通用火箭炮点火控制系统,实现了火箭炮点火控制的自动化。论文阐述了高低压发射系统的原理,在确定了高低压发射系统总体设计方案之后,对高低压发射系统的各子系统进行了分析和初步设计,其中包括高低压系统喷管设计和高低压定向器设计等。针对多管火箭炮装填速度与装填可靠性之间的矛盾和难题,提出了采用箱式发射技术实现多管火箭炮整箱装填的设计方案,较全面地研究了该装填系统涉及到的技术难点,采用控制的电液比例技术解决了液压缸快速运行与高精度定位。
同时,本文应用多刚体系统动力学理论及虚拟样机技术,对多管火箭炮进行了发射特性仿真分析,并对火箭炮箱式发射定向器进行了研究分析。并通过计算求的该结构设计较好的提高火箭弹发射的密集度。
本论文的工作为近程反导多管火箭炮武器的设计和进一步研究提供了一定的设计基础和理论依据,论文设计的研究方法将对今后的相关研究提供新的思路和手段。
Along with the rapid development of the world military technology, rocket weapon is endued with new mission namely that aerial defense. The concept of short-range and anti-missile MBRL is put forward based on the campaign requirements analysis and equipment requirements analysis of the weapon, some function, structure and performance of the weapon are analyzed, and these subsystems have been designed.
The analog and digital electricity technique, communication technique,control technique and SCM technique can be used to study the frame of the ignition and control system. The composition of the hadware system, the control and application software system, and the rocket launcher ignition and control system adapting to different number of tubes has be developed. This system realized automation of the ignition and control of rocket launcher. This thesis expounds the principle of high-low launch system, after the establishment of collectivity design project of high-low system, it researches and designs all subsystem of rocket launch system, such as high-low nozzle design, launching guider design. The dissertation sets forth the design scenario of holistic container loading rising container fire technology against the contradiction between the MRL loading speed and reliability; and carrier out a three-dimensional study of the tough points that the loading system cover; realizes the fast movement of the hydro-cylinder and the highly accurate positioning by way of the PLC-based electro-hydraulic proportion control technology.
At the same time, launching characteristic simulation for designing multiply rocket launch system is conducted using multi-tigid-body dynamic theories and visual prototype technology. The dynamic analysis investigation of guider pipe is done using momentum finite element method. Though calculating, the close grouping of shots after the structure design is better than convertional rocket weapon system.
In summary, this thesis’s work provides foundation and theory gist for further researches about short range and antimissile MBRL system, and the research methods provides new thoughts and means for correlative research.
本文将模拟和数字电子技术、数据通信、控制技术、单片机技术综合应用于火箭炮点火控制系统的设计,通过对控制系统的结构、构成及应用的深入研究,成功的设计了适用不同管数的通用火箭炮点火控制系统,实现了火箭炮点火控制的自动化。论文阐述了高低压发射系统的原理,在确定了高低压发射系统总体设计方案之后,对高低压发射系统的各子系统进行了分析和初步设计,其中包括高低压系统喷管设计和高低压定向器设计等。针对多管火箭炮装填速度与装填可靠性之间的矛盾和难题,提出了采用箱式发射技术实现多管火箭炮整箱装填的设计方案,较全面地研究了该装填系统涉及到的技术难点,采用控制的电液比例技术解决了液压缸快速运行与高精度定位。
同时,本文应用多刚体系统动力学理论及虚拟样机技术,对多管火箭炮进行了发射特性仿真分析,并对火箭炮箱式发射定向器进行了研究分析。并通过计算求的该结构设计较好的提高火箭弹发射的密集度。
本论文的工作为近程反导多管火箭炮武器的设计和进一步研究提供了一定的设计基础和理论依据,论文设计的研究方法将对今后的相关研究提供新的思路和手段。
Along with the rapid development of the world military technology, rocket weapon is endued with new mission namely that aerial defense. The concept of short-range and anti-missile MBRL is put forward based on the campaign requirements analysis and equipment requirements analysis of the weapon, some function, structure and performance of the weapon are analyzed, and these subsystems have been designed.
The analog and digital electricity technique, communication technique,control technique and SCM technique can be used to study the frame of the ignition and control system. The composition of the hadware system, the control and application software system, and the rocket launcher ignition and control system adapting to different number of tubes has be developed. This system realized automation of the ignition and control of rocket launcher. This thesis expounds the principle of high-low launch system, after the establishment of collectivity design project of high-low system, it researches and designs all subsystem of rocket launch system, such as high-low nozzle design, launching guider design. The dissertation sets forth the design scenario of holistic container loading rising container fire technology against the contradiction between the MRL loading speed and reliability; and carrier out a three-dimensional study of the tough points that the loading system cover; realizes the fast movement of the hydro-cylinder and the highly accurate positioning by way of the PLC-based electro-hydraulic proportion control technology.
At the same time, launching characteristic simulation for designing multiply rocket launch system is conducted using multi-tigid-body dynamic theories and visual prototype technology. The dynamic analysis investigation of guider pipe is done using momentum finite element method. Though calculating, the close grouping of shots after the structure design is better than convertional rocket weapon system.
In summary, this thesis’s work provides foundation and theory gist for further researches about short range and antimissile MBRL system, and the research methods provides new thoughts and means for correlative research.
引文
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[39]朱玉川,李志刚,马大为,乐贵高.某箱式多管火箭炮自动装填装置设计.弹箭与制导学报,2006,1:97—99
[40]刘广璞,潘宏侠,姚竹亭.某火炮自动装填机构动作性能试验.太原师范学院学报(自然科学版),2004,6:63—65
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[45]朱玉川.某箱式多管火箭炮快速装填与高精度自动操瞄系统研究.南京理工大学博士论文,2006,11:18—21
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[2]王锋,潘书山,马大为等.弹箭结合武器系统作战效能评估的排队网络方法.弹箭与制导学报,2005,25(3):275—277
[3]潘志刚,王学军.金属风暴武器系统在近程防御中的应用.火力与指挥控制,2007,6
[4]钟志通.现代防空体系发展趋势.飞航导弹,2001,3:32—34
[5]徐国诚.高技术空袭与防空.北京:国防大学出版社,2000
[6]杨华.美国反导系统的发展历史和技术现状.飞航导弹,2001,7:11—15
[7]王晓民.澳大利亚的金属风暴.兵器快报,1998(20):7—8
[8]柴进忠.“金属风暴”与“毒蜘蛛”.国防技术基础。2003(5):6
[9] Metal Storm Technology.2001 Metal Storm Limited. A.C.N. 064 270 006
[10]袁俊.国外巡航导弹技术发展综述.航空兵器,2000,6
[11] Michael 0’Dwyer.Barrel assembly with over pressure relief.USA Patent, 0157526. 2002,2
[12] Boisson D,Legeret G,Rigollet F.Radiative Heat Transfer in a Gun Barrel.Proceedings of 17th International Symposium on Ballistics.Midrans, South Africa.1998: 507—513
[13]赫雷.串联预装填多体系统的结构原理及控制理论研究.南京理工大学硕士学位论文,2003
[14]张春来.近程反导武器系统.舰载武器,2002,1:29—32
[15]戴峰.现代系统工程—大规模决策的思想、过程和方法[M] .郑州:河南人民出版社,1998
[16]王锋.舰载多功能火箭炮系统分析与研究.南京理工大学博士学位论文,2007,4
[17] Dai Longcheng,Xuan Yimin,Liao Zhengqiang.A Method In System Design Of Ejecting Device Of Missiles.Transactions of nanjing University of Aeronautics & Astronautics.2002,6:44—52
[18]赵承庆,姜毅编著.火箭导弹武器系统概论.北京:北京理工大学出版社,1996
[19] Lawrence D. Bacon,Asher H. Sharoni.Crusader is not only option for US Army howitzer.International Defense Review,1995(12):45—50
[20] Christopher F.Foss. More reach for artillery.Jane’s Defense’96:115—119
[21]崔庆忠,冯代英,任慧.几种火箭弹点火具的对比研究.火工品,1998,4:31—34
[22]高明坤,宋廷伦.火箭导弹发射装置构造.北京:北京理工大学出版社,1996.8
[23]姚昌仁,张波.火箭导弹发射装置设计.北京:北京理工大学出版社,1998.9
[24]吴秉贤,严世泽等.火箭发射装置结构分析.北京:国防工业出版社,1988
[25]贺北斗,林永明等.火箭发射装置设计.北京:国防工业出版社,1988
[26]马合林.某多管火箭炮点火控制系统设计.南京理工大学硕士论文,2007,6
[27]陈富安.单片机与可编程控制器应用技术.北京:电子工业出版社,2003.8
[28]马家辰,孙玉德等.MCS-51单片机原理及接口技术.哈尔滨:哈尔滨工业大学出版社,2003.4
[29] RS-485.RS-422 and RS-485 Application note.B&B Electronics Mfg.co.inc.1997
[30] Munro.Modern Approaches to Control Systems Design.New York: Prentice-Hall, Inc.1999
[31]贺北斗.火箭发射系统分析.北京:国防工业出版社,1989
[32]阎太忱等.火炮内弹道学.北京:国防工业出版社,1975
[33] William M. Gray.A study of the possible use of hybrid rocket systems as targets in ballistic missile defense tests.Doctor paper, the University of Alabama in Huntsville, 2002
[34]武小松等.固体火箭发动机气体动力学.北京:国防工业出版社,2005
[35]董师颜等.固体火箭发动机原理.北京:北京理工大学出版社,1996
[36]刘树华等.火箭弹设计.北京:国防工业出版社,1983
[37] Antonino Getal.Virtual Reality As A Tool For Verification Of Assembly And Maintenance Processes.COMPUTER&GRAPHICS, 1999
[38] Y.L.Gu, et al, control of weapon pointing systems based on robotic formulation, Proceedings of the 1992 American Control Conference, Vol.1,1992: 413—418
[39]朱玉川,李志刚,马大为,乐贵高.某箱式多管火箭炮自动装填装置设计.弹箭与制导学报,2006,1:97—99
[40]刘广璞,潘宏侠,姚竹亭.某火炮自动装填机构动作性能试验.太原师范学院学报(自然科学版),2004,6:63—65
[41] Rupert Pengelley , Murray Hammick , Mark Hewish . New Sp artillery developments. International Defense Review,1991(9):929—930
[42] Christopher F. Foss.More reach for artillery.Jane’s Defense’96:115—119
[43] Christopher F. Foss.SP artillery needs greater capability.International Defense Riview, 1995(12):35—43
[44]刘胜,彭侠夫,叶瑰昀编著.现代伺服系统设计.哈尔滨:哈尔滨工程大学出版社,2001,8
[45]朱玉川.某箱式多管火箭炮快速装填与高精度自动操瞄系统研究.南京理工大学博士论文,2006,11:18—21
[46] Rupert Pengelley.Rheinmetall’s Langesrohr“pentalateral”155mm artillery ordnance for the 1990s.International Defense Review,1989(5):653—655
[47]袁士杰,吕哲勤.多刚体系统动力学.北京:北京理工大学出版社,1992
[48] Tokat, Sezai; Eksin, Ibrahim, Guzelkaya, Mujde; Soylemez, M.Design of a sliding mode controller with a nonlinear time-varying sliding surface: Transactions of the Institute of Measurement and Control, v25, n2, 2003:145—162
[49]王良明.弹炮多体系统动力学.力学与实践,1994(5)
[50]洪嘉振.多体系统动力学—理论、计算方法和应用.上海:上海交通大学出版社,1992
[51]陈立平.机械系统动力学分析及ADAMS应用教程.北京:清华大学出版社,2005
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