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Biased retro-proportional navigation law for interception of high-speed targets with angular constraint 被引量:8
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作者 Liang YAN ji-guang zhao +1 位作者 Huai-rong SHEN Yuan LI 《Defence Technology(防务技术)》 SCIE EI CAS 2014年第1期60-65,共6页
A new guidance law, called biased retro proportional navigation(BRPN), is proposed. The guidance law is designed to intercept high-speed targets with angular constraint, which can be used for ballistic target intercep... A new guidance law, called biased retro proportional navigation(BRPN), is proposed. The guidance law is designed to intercept high-speed targets with angular constraint, which can be used for ballistic target interception. BRPN guidance law is defined, and the exact time-varying bias for a required impact angle is derived. Furthermore, the simulation results(trajectory, variation of navigation ratio, capture region, etc) are compared with those of biased proportional navigation(BPN), proportional navigation and retro-proportional navigation. The results show that,at the cost of a higher intercept time, BRPN demands lower terminal lateral acceleration and has larger capture region compared to BPN. 展开更多
关键词 比例导引法 角度约束 拦截 横向加速度 制导律 仿真结果 时间成本 冲击角
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Combined proportional navigation law for interception of high-speed targets 被引量:4
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作者 Yuan LI Liang YAN +2 位作者 ji-guang zhao Fan LIU Tao WANG 《Defence Technology(防务技术)》 SCIE EI CAS 2014年第3期298-303,共6页
A new proportional navigation(PN) guidance law,called combined proportional navigation(CPN),is proposed.The guidance law is designed to intercept high-speed targets,which is a common case for ballistic targets.The ran... A new proportional navigation(PN) guidance law,called combined proportional navigation(CPN),is proposed.The guidance law is designed to intercept high-speed targets,which is a common case for ballistic targets.The range of target-to-interceptor speed ratio during target interception is derived when guidance laws are applied in high-speed targets interception,and the effectiveness of negative navigation ratio in the PN-based guidance law is proven analytically in some lemmas.Based on the lemmas,the lateral acceleration command of CPN is defined,and the solution to the appearance of singularity in time-varying navigation ratio is given.The simulation results show that CPN can determine headon engagement(as PN) or tail-chase engagement(as RPN) through initial path angle compared with PN and retro proportional navigation(RPN),and can adjust the value of navigation ratio for head-on engagement or tail-chase engagement.Therefore,the capture region of CPN is larger than that of other guidance laws using PN-based methods. 展开更多
关键词 COMBINED proportional NAVIGATION Proportional NAVIGATION HIGH-SPEED target CAPTURE region INTERCEPTION
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Growth model of cavity generated by the projectile impacting liquid-filled tank 被引量:3
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作者 Bei-lei zhao ji-guang zhao +2 位作者 Cun-yan Cui Yong-sheng Duan Yan Wang 《Defence Technology(防务技术)》 SCIE EI CAS CSCD 2020年第3期609-616,共8页
The high-speed impact of a projectile on a liquid-filled tank causes the hydraulic ram,in which a cavity is formed.To study the growth characteristics of the cavity,the formation mechanism of the cavity is analyzed.Th... The high-speed impact of a projectile on a liquid-filled tank causes the hydraulic ram,in which a cavity is formed.To study the growth characteristics of the cavity,the formation mechanism of the cavity is analyzed.The effect of Reynolds number and Mach number on drag coefficient is considered,the axial and radial growth models of the cavity are established respectively.The relative errors between the cavity length calculated by the axial growth model,the cavity diameter calculated by the radial growth model and Ma L.Y.test results are less than 20%,which verifies the effectiveness of the axial and radial growth models.Finally,numerical simulation is carried out to study the growth characteristics of the cavity caused by the projectile impacting the satellite tank at the velocity of 4000 m/s.The cavity length and diameter calculated by the axial and radial growth models agree well with those obtained by simulation results,indicating that the cavity length and diameter in satellite tank can be accurately calculated by the axial and radial growth models. 展开更多
关键词 PROJECTILE Impact Liquid-filled tank CAVITY Axial growth model Radial growth model
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