多管火箭火控系统总体技术研究
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摘要
本文通过对某型多管火箭的火控系统总体技术的研究,提出火控系统进行适应性改进的总体方案。
详细论证了火控系统组成、功能及战技指标;研究并建立了多管火箭弹道模型,建立了火箭弹滑轨段、火箭弹离轨到子母战斗部分离、开舱、子弹飞行的弹道模型;火箭炮自动操瞄调炮精度是影响射击精度的重要因素,本文对影响自动操瞄调炮精度的误差源进行了分析研究,导出了它们影响调炮精度的定量关系,并提出了一种可以提高操瞄调炮精度的控制方法,并在实际中得到应用,实际测试结果与理论计算结果较吻合;第五章详细介绍了火控系统工作方式,其中重点论证了作战流程、三种工作方式、接口关系及发控时序的设计;第六章采用高斯投影的方法解决GPS定位定向导航系统给出的美国WGS84坐标系,同我国炮兵目前应用的国家直角平面坐标系不统一的问题。
通过几个方面的研究论证提出的火控系统总体方案,可以满足设计要求。
The synthesis technologies of one kind of MRLS's firing control system were researched on this paper, and the adaptive improvement was provided for overall conception.
Detail demonstration on firing control system' s formation, function and operational performance. The ballistic models on MRLS and the rocket in the parts of glide, separation from cargo, chamber-opening and sub-munitions flight path were created in this paper. The accuracy of gun moving by automatic operation and aiming was the critical factor to influence the precision of rocket and analyst on the error sources which would affect it. The fixed quantity relations which the error sources affect the accuracy of gun moving were derived. Then, a control method which it can raise the accuracy of gun moving was provided, and applied in live system. The results from test were coincided with theoretical calculation. The operation modes of firing control system were introduced in detail in fifth chapter, and the points on operation flow chart, three working models, interface relations and design launch and control time sequences were discussed. The Gauss projection was to solve the GPS provided the co-ordinates in USA WGS84 which the rectangular co-ordinates system applied in our artillery units were not unification.
The overall conceptions of firing control system were discussed in serial plans which can meet the design requesting.
详细论证了火控系统组成、功能及战技指标;研究并建立了多管火箭弹道模型,建立了火箭弹滑轨段、火箭弹离轨到子母战斗部分离、开舱、子弹飞行的弹道模型;火箭炮自动操瞄调炮精度是影响射击精度的重要因素,本文对影响自动操瞄调炮精度的误差源进行了分析研究,导出了它们影响调炮精度的定量关系,并提出了一种可以提高操瞄调炮精度的控制方法,并在实际中得到应用,实际测试结果与理论计算结果较吻合;第五章详细介绍了火控系统工作方式,其中重点论证了作战流程、三种工作方式、接口关系及发控时序的设计;第六章采用高斯投影的方法解决GPS定位定向导航系统给出的美国WGS84坐标系,同我国炮兵目前应用的国家直角平面坐标系不统一的问题。
通过几个方面的研究论证提出的火控系统总体方案,可以满足设计要求。
The synthesis technologies of one kind of MRLS's firing control system were researched on this paper, and the adaptive improvement was provided for overall conception.
Detail demonstration on firing control system' s formation, function and operational performance. The ballistic models on MRLS and the rocket in the parts of glide, separation from cargo, chamber-opening and sub-munitions flight path were created in this paper. The accuracy of gun moving by automatic operation and aiming was the critical factor to influence the precision of rocket and analyst on the error sources which would affect it. The fixed quantity relations which the error sources affect the accuracy of gun moving were derived. Then, a control method which it can raise the accuracy of gun moving was provided, and applied in live system. The results from test were coincided with theoretical calculation. The operation modes of firing control system were introduced in detail in fifth chapter, and the points on operation flow chart, three working models, interface relations and design launch and control time sequences were discussed. The Gauss projection was to solve the GPS provided the co-ordinates in USA WGS84 which the rectangular co-ordinates system applied in our artillery units were not unification.
The overall conceptions of firing control system were discussed in serial plans which can meet the design requesting.
引文
[1]火箭炮的发展及性能提高的途径.北京:导弹与航天运载技术,1988.
[2]《外军多管火箭炮的装备现状、技术水平及特点》.外军炮兵,2001,2:3-12.
[3]《多管火箭系统的现状与未来》.飞航导弹,1999,10:10-13.
[4]《俄罗斯新兵器手册》.北京:兵器工业版社.1998.3:610-614.
[5]杨培根.火力控制系统总论.第1版.北京:兵器工业出版社,1998.
[6]李润山,赵志江.世界多管火箭武器的发展现状及发展趋势研究.西安:弹箭技术,1998.
[7]《JANE'S ARMOUR AND ARTILLERY}.2002-2003:795-878.
[8]Peter Bilello Lockheed Martin Miss]1e and Fire Control.1999.
[9]董志荣.论指挥控制系统发展-过去、现在和未来.北京:舰船科学技术,1997.
[10]康敏译.国外野战火炮火控系统.北京:火炮科技信息,2002,5:22-24.
[11]殷国发等.数据融合技术在C~3I系统的应用.太原:火力与指挥控制,2002.
[12]张安等.航空综合火力控制原理.第1版.北京:1997.
[13]谢锡祺.自动控制理论基础.第2版.北京:北京理工大学出版社,1992.
[14]浦发.外弹道学.第1版.北京:国防工业出版社,1980.
[15]宁新建.火控系统中的容错技术分析.情报指挥系统与仿真.2002.
[16]孙永荣等.GPS多天线数据采集与控制系统.火炮科技信息,2003.
[17]贾沛然.远程火箭弹道学.第1版.长沙:国防科技大学出版社,1993.
[18]陆彦.航空火力控制技术.第1版.北京:国防工业出版社,1994.
[19]郭锡福、赵子华.火控弹道模犁理论及应用.第1版.北京:国防工业出版社,1997.
[20]朱元昌.火控系统的数学仿真.第2版.北京:国防工业出版社,1997.
[21]陈世年等.控制系统设计.第1版.北京:宁航出版社,1996.
[22]文仲辉.导弹武器系统分析.第1版.北京:北京理工大学,1998.
[23]北京理工大学.远程多管火箭炮武器系统发射顺序和发射间隔仿真报告,1998.
[24]徐明友.火箭外弹道学.第1版.北京:兵器工业出版社 1989.
[25]陶化成.压制兵器自动操瞄系统的精度分析.火力与指挥系统,1991,18(3).
[26]张赤军,马宏.火箭炮多参数的综合测量.兵工学报,2007,28(3):374-376.
[27]郭治.现代火控系统.第1版.北京:国防工业出版社,1996.
[28]付庆宏,赵洪荣.一种克服火控系统假定误差的方法.火力指挥与控制,2002,27(3):21-22
[29]卢集龙.火控与火控设计原理.第1版.北京:国防工业出版社,1985.
[30]侯凯,牛竹云.火控系统精度分配研究.火力与指挥控制96学术论文集,太原,1996.
[31]孔祥元、郭际明、刘宗全.大地测量学基础.第1版.武汉:武汉大学出版社,2001.
[32]徐中信.远程多管火箭武器系统装备与发展[C].火箭导弹学会学术会议论文集,1995,9.
[33]刘明喜.火箭武器系统弹道及密集度研究[C].火箭导弹学会学术会议论文集,2002年.
[34]孔炜,朱春梅著.火箭发射起始扰动仿真研究[J].火炮发射与控制学报,1998.
[35]P.P.贝文顿著.仇维礼等译.数据处理和误差分析[M]知.第1版.北京:识出版社,1986.
[36]贾沛璋.误差分析与数据处理[M].第1版.北京:国防工业出版社,1992.
[37]姚昌仁,张波著.火箭导弹发射装置设计[C].火箭导弹学会学术会议论文集,1998年.
[2]《外军多管火箭炮的装备现状、技术水平及特点》.外军炮兵,2001,2:3-12.
[3]《多管火箭系统的现状与未来》.飞航导弹,1999,10:10-13.
[4]《俄罗斯新兵器手册》.北京:兵器工业版社.1998.3:610-614.
[5]杨培根.火力控制系统总论.第1版.北京:兵器工业出版社,1998.
[6]李润山,赵志江.世界多管火箭武器的发展现状及发展趋势研究.西安:弹箭技术,1998.
[7]《JANE'S ARMOUR AND ARTILLERY}.2002-2003:795-878.
[8]Peter Bilello Lockheed Martin Miss]1e and Fire Control.1999.
[9]董志荣.论指挥控制系统发展-过去、现在和未来.北京:舰船科学技术,1997.
[10]康敏译.国外野战火炮火控系统.北京:火炮科技信息,2002,5:22-24.
[11]殷国发等.数据融合技术在C~3I系统的应用.太原:火力与指挥控制,2002.
[12]张安等.航空综合火力控制原理.第1版.北京:1997.
[13]谢锡祺.自动控制理论基础.第2版.北京:北京理工大学出版社,1992.
[14]浦发.外弹道学.第1版.北京:国防工业出版社,1980.
[15]宁新建.火控系统中的容错技术分析.情报指挥系统与仿真.2002.
[16]孙永荣等.GPS多天线数据采集与控制系统.火炮科技信息,2003.
[17]贾沛然.远程火箭弹道学.第1版.长沙:国防科技大学出版社,1993.
[18]陆彦.航空火力控制技术.第1版.北京:国防工业出版社,1994.
[19]郭锡福、赵子华.火控弹道模犁理论及应用.第1版.北京:国防工业出版社,1997.
[20]朱元昌.火控系统的数学仿真.第2版.北京:国防工业出版社,1997.
[21]陈世年等.控制系统设计.第1版.北京:宁航出版社,1996.
[22]文仲辉.导弹武器系统分析.第1版.北京:北京理工大学,1998.
[23]北京理工大学.远程多管火箭炮武器系统发射顺序和发射间隔仿真报告,1998.
[24]徐明友.火箭外弹道学.第1版.北京:兵器工业出版社 1989.
[25]陶化成.压制兵器自动操瞄系统的精度分析.火力与指挥系统,1991,18(3).
[26]张赤军,马宏.火箭炮多参数的综合测量.兵工学报,2007,28(3):374-376.
[27]郭治.现代火控系统.第1版.北京:国防工业出版社,1996.
[28]付庆宏,赵洪荣.一种克服火控系统假定误差的方法.火力指挥与控制,2002,27(3):21-22
[29]卢集龙.火控与火控设计原理.第1版.北京:国防工业出版社,1985.
[30]侯凯,牛竹云.火控系统精度分配研究.火力与指挥控制96学术论文集,太原,1996.
[31]孔祥元、郭际明、刘宗全.大地测量学基础.第1版.武汉:武汉大学出版社,2001.
[32]徐中信.远程多管火箭武器系统装备与发展[C].火箭导弹学会学术会议论文集,1995,9.
[33]刘明喜.火箭武器系统弹道及密集度研究[C].火箭导弹学会学术会议论文集,2002年.
[34]孔炜,朱春梅著.火箭发射起始扰动仿真研究[J].火炮发射与控制学报,1998.
[35]P.P.贝文顿著.仇维礼等译.数据处理和误差分析[M]知.第1版.北京:识出版社,1986.
[36]贾沛璋.误差分析与数据处理[M].第1版.北京:国防工业出版社,1992.
[37]姚昌仁,张波著.火箭导弹发射装置设计[C].火箭导弹学会学术会议论文集,1998年.