| 末段修正迫弹脉冲发动机控制策略 |
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| 引用本文： | 姚文进,王晓鸣,李文彬,高旭东.末段修正迫弹脉冲发动机控制策略[J].探测与控制学报,2008,30(Z1). |
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| 作者姓名： | 姚文进 王晓鸣 李文彬 高旭东 |
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| 作者单位： | 南京理工大学机械工程学院,江苏,南京,210094 |
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| 摘 要： | 针对迫弹的末段弹道修正问题,建立了脉冲控制的六自由度弹道模型,提出了一种基于实时弹目偏差量的控制策略,仿真研究了该控制策略对修正能力、飞行稳定性的影响规律等问题.结果表明:该控制策略能有效地修正弹道,缩小弹目偏差.该研究对脉冲发动机在末段修正迫弹上的工程应用有一定的参考.
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| 关 键 词： | 脉冲修正 控制策略 弹目偏差 |
The Control Strategy of Pulse Engine in Terminal Correction Mortar |
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| YAO Wen-jin,WANG Xiao-ming,LI Wen-bin,GAO Xu-dong.The Control Strategy of Pulse Engine in Terminal Correction Mortar[J].Journal of Detection & Control,2008,30(Z1). |
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| Authors: | YAO Wen-jin WANG Xiao-ming LI Wen-bin GAO Xu-dong |
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| Affiliation: | YAO Wen-jin,WANG Xiao-ming,LI Wen-bin,GAO Xu-dong (School of Mechanical Engineering,Nanjing University of Science , Technology,Nanjing 210094,China) |
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| Abstract: | In view of the problem of the terminal trajectory correction mortar,the 6 degree of freedom trajectory correction model using impulse was established.One control strategy based on the miss distance between projectile and target is put forward.Based on trajectory model,effect of this control strategy on the correction ability and flight stability was studied in this paper.The simulation result indicates that this control strategy can correct the trajectory effectively and reduce the miss distance between pro... |
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| Keywords: | pulse correction control strategy miss distance |
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