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空天防御  2019, Vol. 2 Issue (1): 37-41    
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  导航制导与控制技术 本期目录 | 过刊浏览 | 高级检索 |
基于变结构的空间杀伤器末制导律研究
臧月进, 李仁俊, 曾亮
上海机电工程研究所, 上海 201109
Research on Terminal Guidance Law for Space Kill Vehicle Based on Variable Structure
ZANG Yuejin, LI Renjun, ZENG Liang
Shanghai Electro-Mechanical Engineering Institute, Shanghai 201109, China
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摘要 针对空间杀伤器高速交会条件下的末制导问题,首先在建立空间杀伤器动力学模型的基础上,基于相对运动方程设计了采用指数趋近律的变结构制导律,然后进行了平滑处理以抑制系统抖动,最后采用Schmitt触发器对制导指令进行了脉宽调制。仿真结果表明: 针对空间目标杀伤变结构制导律具有鲁棒性强、脱靶量小和燃料消耗低的优势,证明了该方法的有效性。
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Abstract:The terminal guidance law for space kill vehicle in high-speed encounter was studied. Firstly, dynamic models of space kill vechicle were established. Then the variable structure guidance law was designed adopting exponential approach law based on the relative motion equation, and chattering was weakened through smoothing. Lastly, pulse width modulation was conducted for guidance command by Schmitt Trigger. The simulation results showed that the guidance law against space target presented in this paper was effective, which had the merits: strong robustness, small miss distance, and low fuel consumption.
收稿日期: 2018-07-09      出版日期: 2019-01-14
ZTFLH:  V414.1  
基金资助:上海市自然科学基金(编号16ZR1415900)
作者简介: 臧月进(1987— ),男,硕士,工程师,主要研究方向为飞行器制导控制系统。
引用本文:   
臧月进, 李仁俊, 曾亮. 基于变结构的空间杀伤器末制导律研究[J]. 空天防御, 2019, 2(1): 37-41.
ZANG Yuejin, LI Renjun, ZENG Liang. Research on Terminal Guidance Law for Space Kill Vehicle Based on Variable Structure. Air & Space Defense, 2019, 2(1): 37-41.
链接本文:  
https://www.qk.sjtu.edu.cn/ktfy/CN/      或      https://www.qk.sjtu.edu.cn/ktfy/CN/Y2019/V2/I1/37

参考文献
[1] 杨帆, 李小林, 刘小波, 傅建明. 基于特征线理论的超声速进气道压缩面设计研究[J]. 空天防御, 2019, 2(1): 22-28.
[2] 臧月进, 李仁俊, 安国琛. 大气层外反TBM拦截弹变结构末制导律研究[J]. 空天防御, 2018, 1(2): 22-26.
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