考虑视场角约束下的攻击时间控制制导律
Impact-time-control Guidance Law Considering Field-of-view Constraint
查看参考文献13篇
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文摘
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为了实现视场角约束下的攻击时间控制,基于导弹-目标相对运动模型,对考虑视场角约束下的攻击时间控制制导问题开展了研究。建立了以攻击时间误差和前置角收敛到0为准则的攻击时间控制模型。在比例导引法的基础上,采用附加偏置控制项的形式,在考虑视场角约束条件下设计了无奇点的攻击时间控制制导律。该制导律具有一定的最优性,攻击时间误差先于前置角收敛到0,制导加速度指令最终也收敛为0。采用Lyapunov稳定性理论,证明了该攻击时间控制制导律的稳定性。仿真结果表明,该制导律能够有效实现视场角约束下的攻击时间控制。 |
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其他语种文摘
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In order to achieve impact time control with field-of-view constraint, the problem of impact time control guidance with field-of-view constraint was studied based on relative motion model of missile-target. The model was established according to the criterion of the impact time error and leading angle of missle converging to zero. Based on the proportional navigation,a nonsingular impact-time-control guidance law with field-of-view constraint was designed by using the form of additional bias control. The guidance law has certain optimality. The impact time error converges to zero before the leading angle converges to zero, and the guidance commande finally converges to zero. The stability of impact-time-control guidance law was proved by using Lyapunov stability theory. Simulation results show that the guidance law can effectively achieve the impact time control under the constraint of field-of-view. |
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来源
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弹道学报
,2018,30(4):7-12 【核心库】
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DOI
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10.12115/j.issn.1004-499x(2018)04-002
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关键词
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导弹
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攻击时间控制
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比例导引法
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视场角约束
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地址
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1.
南京理工大学能源与动力工程学院, 江苏, 南京, 210094
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西北工业集团有限公司设计二所, 陕西, 西安, 710043
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语种
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中文 |
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文献类型
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研究性论文 |
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ISSN
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1004-499X |
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学科
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武器工业 |
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基金
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国家自然科学基金项目
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中国博士后科学基金
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文献收藏号
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CSCD:6397974
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