OALib Journal期刊
基于相对速度偏角的舰空导弹三维制导律设计
, PP. 54-58
Keywords: 舰空导弹 ,制导律 ,相对速度 ,变结构控制 ,鲁棒性
Abstract:
针对舰空导弹拦截掠海飞行目标问题,考虑到目标具有强机动性和导引头对低空海面目标的视线角速度量测噪声,以及末制导在三维空间中进行,在建立空间导弹拦截目标相对运动模型基础上,选择空间导弹和目标的相对速度偏角作为零化目标,设计了一种具有强鲁棒性的基于零化相对速度偏角的空间变结构末制导律,给出了导引指令信息解算模型,仿真结果不仅验证了解算模型的正确性,还表明了在对抗目标大机动和低空目标视线角速度量测噪声等方面,所设计导引律比传统的空间末制导律具有更强的鲁棒性.
References
[1] 周荻.寻的导弹新型导引规律[M].北京:国防工业出版社,2002.ZHOU Di.Novelguidancelaw for homing missile[M].Beijing:NationalDefenseIndustryPress,2002.(inChinese) [2] 张友安,胡云安.导弹控制和制导的非线性设计方法[M].北京:国防工业出版社,2003:154-162.ZHANGYou-an,HUYun-an.Nonlineardesignapproachesformissilecontrolandguidance[M].Beijing:NationalDefenseIndustryPress,2003:154-162.(inChinese) [3] BYUNGSK,JANG GL,HYUNGSH.BiasedPNGlawforimpact with angularconstraint[J].IEEE TransactionsonAerospaceandElectronicSystems,1998,34(1):277-288. [4] TALS,MOSHEI,ODED M G.Sliding modecontrolforintegrated missileautopilot-guidance[C].AIAA Guidance,Navigation,andControlConferenceandExhibit.Providence,RhodeIsland:AIAA,2004:1-18. [5] TALS.Optimalcooperativepursuitandevasionstrategiesagainstahomingmissile[J].JournalofGuidance,ControlandDynamics,2011,34(2):414-425. [6] 宋建梅,张天桥.带末端落角约束的变结构导引律[J].弹道学报,2001,13(1):16-20.SONG Jian-mei,ZHANG Tian-qiao.The passive homingmissile’s variable structure proportional navigation withterminalimpactangularconstraint[J].JournalofBallistics,2001,13(1):16-20.(inChinese) [7] YU Xing-huo,MAN Zhi-hong.Fastterminalsliding modecontroldesignfornonlineardynamicalsystems[J].IEEETransactionsonCircuitsandSystemsI:FundamentalTheoryandApplications,2004,49(2):261-265. [8] JONGKI M,KISEOK K,YOUDAN K.Design of missileguidancelaw viavariablestructurecontrol[J].JournalofGuidance,ControlandDynamics,2001,24(4):659-664. [9] 张友安,胡云安,苏身榜.一种基于变结构控制的鲁棒制导算法设计[J].系统工程与电子技术,2001,23(4):61-63.ZHANG You-an,HU Yun-an,SU Shen-bang.A robustguidancealgorithmdesignusingvariablestructurecontrol[J].SystemsEngineeringandElectronics,2001,23(4):61-63.(inChinese) [10] 郭鸿武,林维菘,刘明俊.基于相对速度偏角的变结构导引律[J].宇航学报,2001,22(3):33-37.GUO Hong-wu,LIN Wei-song,LIU Ming-jun.A variablestructureguidancelaw basedonrelativevelocitydeflectionangle[J].JournalofAstronautics,2001,22(3):33-37.(inChinese) [11] 林嘉新,赵永涛,胡云安.一种基于零化相对速度偏角的变结构末制导律设计[J].海军航空工程学院学报,2009,24(6):646-650.LINJia-xin,ZHAOyong-tao,HUYun-an.Designofavariablestructureterminalguidancelaw based on relative velocitydeflection angle [J].Journal of Naval Aeronautical andAstronauticalUniversity,2009,24(6):646-650.(inChinese)
Full-Text
Contact Us
service@oalib.com
QQ:3279437679
WhatsApp +8615387084133
