直升机船台辅助降落模型研究
|
摘要
随着海洋争夺战向立体化,多层化发展,各国迫切需要掌握海上制空权,制海权,维护海洋权益,保障领土安全。由于直升机可担负侦察、搜救、运输、反潜、两栖突击、空中预警以及电子战、水雷战等多种使命,因此,世界各国在竞相发展航空母舰和大型舰船的同时,都在大力发展性能优良的直升机。而建立一套完善的直升机船台辅助降落系统是当前迫切需要解决的主要问题。
本文针对直升机船台辅助降落问题,设计出了一套确定飞机定位及飞行姿态的方法,并进行了模拟仿真。
通过研究本论题的背景和意义和国内外研究的现状,说明研究直升机助降系统的必要性。在直升机助降系统的方案中,主要介绍系统的组成、功能、工作原理,工作流程,和船面的主要设施、降落过程、降落因素等。随后建立直升机辅助降落的数学模型方法,主要论述飞机降落时,确定其位置坐标的方法和飞行姿态,以及飞机飞行中姿态控制原理,偏航控制原理、俯仰控制原理、滚转控制原理及与迎角的关系等。最后,对系统模型进行了模拟仿真,并对其效果进行了简要的评价,分析了系统的优点和存在的不足,指出研究直升机船台辅助降落系统的重要意义。
With the stereoscopic and multipolar development of modern sea battle, every country need master aeroamphibious right urgently to protect sea rights and interests, guarantee territory safety. AS soon as helicopters are concerned, they can take on a good many tasks, such as spy, search and rescue, transport, antisubmarine, amphibious landing sudden attackair early warning and the electronics wars, the torpedo war etc. various mission, therefore, international community at the time of developing the carrier and other ships competitively, all at develop the good ship of function to carry the helicopter strongly. But at present the main and will be resolved urgently problem is to build up a set of perfect helicopter landing system.
This article designs a way for helicopter orient- ion and fly pose, at the same time makes an imitation for test.
It introduces background and meaning of this thesis, including native or foreign research actuality, the necessary of the ship helicopter landing system. It introduces a project for ship helicopter landing system, including system composing, function, working theory, working flow, main establishment on board, landing course, landing factor etc. It recommends one maths model way for ship helicopter landing system. It mainly introduces a means for ship helicopter position coordinate and fly pose when it will land. At the same time it recommends fly pose control theory, Yawing-angle control theory, pitching-angle control theory, turn-angle control theory, meet-angle relation when it is flying. At last, it simulates in systems, estimates the effect, make an analysis of the merit and the flaw and points out the important meaning of the ship helicopter landing system.
本文针对直升机船台辅助降落问题,设计出了一套确定飞机定位及飞行姿态的方法,并进行了模拟仿真。
通过研究本论题的背景和意义和国内外研究的现状,说明研究直升机助降系统的必要性。在直升机助降系统的方案中,主要介绍系统的组成、功能、工作原理,工作流程,和船面的主要设施、降落过程、降落因素等。随后建立直升机辅助降落的数学模型方法,主要论述飞机降落时,确定其位置坐标的方法和飞行姿态,以及飞机飞行中姿态控制原理,偏航控制原理、俯仰控制原理、滚转控制原理及与迎角的关系等。最后,对系统模型进行了模拟仿真,并对其效果进行了简要的评价,分析了系统的优点和存在的不足,指出研究直升机船台辅助降落系统的重要意义。
With the stereoscopic and multipolar development of modern sea battle, every country need master aeroamphibious right urgently to protect sea rights and interests, guarantee territory safety. AS soon as helicopters are concerned, they can take on a good many tasks, such as spy, search and rescue, transport, antisubmarine, amphibious landing sudden attackair early warning and the electronics wars, the torpedo war etc. various mission, therefore, international community at the time of developing the carrier and other ships competitively, all at develop the good ship of function to carry the helicopter strongly. But at present the main and will be resolved urgently problem is to build up a set of perfect helicopter landing system.
This article designs a way for helicopter orient- ion and fly pose, at the same time makes an imitation for test.
It introduces background and meaning of this thesis, including native or foreign research actuality, the necessary of the ship helicopter landing system. It introduces a project for ship helicopter landing system, including system composing, function, working theory, working flow, main establishment on board, landing course, landing factor etc. It recommends one maths model way for ship helicopter landing system. It mainly introduces a means for ship helicopter position coordinate and fly pose when it will land. At the same time it recommends fly pose control theory, Yawing-angle control theory, pitching-angle control theory, turn-angle control theory, meet-angle relation when it is flying. At last, it simulates in systems, estimates the effect, make an analysis of the merit and the flaw and points out the important meaning of the ship helicopter landing system.
引文
[1]戴自立,现代舰载作战系统,北京:兵器工业出版社,1990,121～122
[2]焦方金,靳红生,浅谈舰载战斗机的降落,舰载武器,2005,(6):82～85
[3]李杰,于川,航空母舰的舰载机着舰装备,现代军事,2006,(10):56～58
[4]陈新民,舰载直升机及其载舰,海军出版社,1986,2～10
[5]孙文胜,毕玉泉,白春华,舰载直升机的舰面效应研究,航空计算技术,2006,36(2):9～12
[6]曹喜金,国外反潜直升机的发展,直升机技术,2003,(3):47～50
[7]张广林,张慧,舰载直升机:“海空轻骑兵”,科技潮,2007,(6):44～45
[8]蒋新桐,中国民用直升机的发展,中国工程科学,2000,2(7):10～15
[9]孙杰,浅谈舰载直升机的海上试飞,飞行力学,2001,19(3):66～69
[10]秦超敏,张西,直升机横侧稳定性试飞数据计算法,飞行力学,1998, 16(1):70～73
[11] Kirkpatrick S.,Gelatt C.D.,Vecchi M.P.,Optimization by simulated annealing,Science,1983,220 (5) :671～680
[12]汪德虎,谭周寿,王建明等,舰炮射击基础理论,北京:海潮出版社,1998,28～29
[13]吕学富,飞行器飞行力学,西安:西北工业大学出版社,1995,55～57
[14] Michael D.G.,高等工程数学,北京:电子工业出版社,2004,65～66
[15]刘玉琏,傅沛仁,数学分析讲义,北京:高等教育出版社,1998,111～113
[16]林永祥,陈明逵,计算方法教程,西安:西安交通大学出版社,2005, 87～88
[17]吕林根,许子道,空间解析几何,北京:高等教育出版,1998,34～37
[18]李金,于秀萍,软件技术及应用,哈尔滨:哈尔滨工程大学出版社,1999,21～28
[19]冯巧玲,自动控制原理,北京:北京航空航天大学出版社,2003,71～75
[20] Simon D. , El-Sherief H. , Real-time Navigation Using Global Positioning System,Aerospace and Electronic Systems Magazine,1995,10(1):31～37
[21] Paul G. .S.,Strapdown Inertial Navigation integration algorithm Designed,Journal of Guidance control and Dynamics,1998,21(2):208～221
[22] Blackman,Samuel S.,Design and Analysis of modern Tracking System, Boston:Arteth House,1999,385～391
[23]朱自谦,一种用于机动目标跟踪的新自适应卡尔曼滤波算法,航空学报,1992,13(4):180～187
[24]董志荣,论信息融合,情报指挥控制系统与仿真技术,2001,(7):21～35
[25]董志荣,论跟踪雷达与火控设备的综合,火力与指挥控制,2000, 25(3):3～4
[26]王本颜,方蕴昌,数据结构技术,北京:清华大学出版社,1988,66～73
[27]窦延平,霍义兴,数据结构教程,上海:上海交通大学出版社,1990, 18～22
[28]傅惠民,仿真结果统计检验方法,机械强度,2005,27(5):598～603
[2]焦方金,靳红生,浅谈舰载战斗机的降落,舰载武器,2005,(6):82～85
[3]李杰,于川,航空母舰的舰载机着舰装备,现代军事,2006,(10):56～58
[4]陈新民,舰载直升机及其载舰,海军出版社,1986,2～10
[5]孙文胜,毕玉泉,白春华,舰载直升机的舰面效应研究,航空计算技术,2006,36(2):9～12
[6]曹喜金,国外反潜直升机的发展,直升机技术,2003,(3):47～50
[7]张广林,张慧,舰载直升机:“海空轻骑兵”,科技潮,2007,(6):44～45
[8]蒋新桐,中国民用直升机的发展,中国工程科学,2000,2(7):10～15
[9]孙杰,浅谈舰载直升机的海上试飞,飞行力学,2001,19(3):66～69
[10]秦超敏,张西,直升机横侧稳定性试飞数据计算法,飞行力学,1998, 16(1):70～73
[11] Kirkpatrick S.,Gelatt C.D.,Vecchi M.P.,Optimization by simulated annealing,Science,1983,220 (5) :671～680
[12]汪德虎,谭周寿,王建明等,舰炮射击基础理论,北京:海潮出版社,1998,28～29
[13]吕学富,飞行器飞行力学,西安:西北工业大学出版社,1995,55～57
[14] Michael D.G.,高等工程数学,北京:电子工业出版社,2004,65～66
[15]刘玉琏,傅沛仁,数学分析讲义,北京:高等教育出版社,1998,111～113
[16]林永祥,陈明逵,计算方法教程,西安:西安交通大学出版社,2005, 87～88
[17]吕林根,许子道,空间解析几何,北京:高等教育出版,1998,34～37
[18]李金,于秀萍,软件技术及应用,哈尔滨:哈尔滨工程大学出版社,1999,21～28
[19]冯巧玲,自动控制原理,北京:北京航空航天大学出版社,2003,71～75
[20] Simon D. , El-Sherief H. , Real-time Navigation Using Global Positioning System,Aerospace and Electronic Systems Magazine,1995,10(1):31～37
[21] Paul G. .S.,Strapdown Inertial Navigation integration algorithm Designed,Journal of Guidance control and Dynamics,1998,21(2):208～221
[22] Blackman,Samuel S.,Design and Analysis of modern Tracking System, Boston:Arteth House,1999,385～391
[23]朱自谦,一种用于机动目标跟踪的新自适应卡尔曼滤波算法,航空学报,1992,13(4):180～187
[24]董志荣,论信息融合,情报指挥控制系统与仿真技术,2001,(7):21～35
[25]董志荣,论跟踪雷达与火控设备的综合,火力与指挥控制,2000, 25(3):3～4
[26]王本颜,方蕴昌,数据结构技术,北京:清华大学出版社,1988,66～73
[27]窦延平,霍义兴,数据结构教程,上海:上海交通大学出版社,1990, 18～22
[28]傅惠民,仿真结果统计检验方法,机械强度,2005,27(5):598～603