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空射倾斜转弯导弹制导控制系统设计 被引量:4
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作者 张友安 张友根 邓以高 《海军航空工程学院学报》 2005年第3期349-352,共4页
讨论了空射BTT导弹的制导命令的生成,特别是针对纵向通道降高问题,设计了一种新的降高段控制指令,然后给出了三个通道的PID控制器.六自由度的仿真结果表明这种制导控制设计是成功的.
关键词 BTT 高度控制 制导命令 过载控制 空射导弹
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Improved differential geometric guidance commands for endoatmospheric interception of high-speed targets 被引量:22
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作者 LI KeBo CHEN Lei TANG GuoJin 《Science China(Technological Sciences)》 SCIE EI CAS 2013年第2期518-528,共11页
Pure proportional navigation(PPN) is suitable for endoatmospheric interceptions,for its commanded acceleration is perpendicular to interceptor velocity.However,if the target is much faster than the interceptor,the hom... Pure proportional navigation(PPN) is suitable for endoatmospheric interceptions,for its commanded acceleration is perpendicular to interceptor velocity.However,if the target is much faster than the interceptor,the homing performance of PPN will be degraded badly.True proportional navigation(TPN) does not have this problem,but its commanded acceleration is perpendicular to the line of sight(LOS),which is not suitable for endoatmospheric interceptions.The commanded acceleration of differential geometric guidance commands(DGGC) is perpendicular to the interceptor velocity,while the homing performance approximates the LOS referenced guidance laws(PPN series).Therefore,DGGC is suitable for endoatmospheric interception of high-speed targets.However,target maneuver information is essential for the construction of DGGC,and the guidance commands are complex and may be without robustness.Through the deep analysis of three-dimensional engagement,a new construction method of DGGC is proposed in this paper.The target maneuver information is not needed any more,and the robustness of DGGC is guaranteed,which makes the application of DGGC possible. 展开更多
关键词 differential geometric guidance commands endoatmospheric interception high-speed targets proportional navigation ROBUSTNESS
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