[1]陈升富,刘 丹,常思江.考虑视场角约束下的攻击时间控制制导律[J].弹道学报,2018,(04):7.[doi:10.12115/j.issn.1004-499X(2018)04-002]
 CHEN Shengfu,LIU Dan,CHANG Sijiang.Impact-time-control Guidance Law Considering Field-of-view Constraint[J].Journal Of Ballistics,2018,(04):7.[doi:10.12115/j.issn.1004-499X(2018)04-002]
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考虑视场角约束下的攻击时间控制制导律()
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《弹道学报》[ISSN:1004-499x/CN:32-1343/TJ]

卷:
期数:
2018年04期
页码:
7
栏目:
出版日期:
2018-12-31

文章信息/Info

Title:
Impact-time-control Guidance Law Considering Field-of-view Constraint
文章编号:
1004-499X(2018)04-0007-06
作者:
陈升富1刘 丹2常思江1
1.南京理工大学 能源与动力工程学院,江苏 南京 210094; 2.西北工业集团有限公司 设计二所,陕西 西安 710043
Author(s):
CHEN Shengfu1LIU Dan2CHANG Sijiang1
1.School of Energy and Power Engineering,Nanjing University of Science and Technology,Nanjing 210094,China; 2. The Second Design Department,Northwest Industrial Group Corporation,Xi’an 710043,China
关键词:
导弹 攻击时间控制 比例导引法 视场角约束
Keywords:
missile impact time control proportional navigation field-of-view constraint
分类号:
TJ303.4
DOI:
10.12115/j.issn.1004-499X(2018)04-002
文献标志码:
A
摘要:
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。
Abstract:
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.

参考文献/References:

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备注/Memo

备注/Memo:
收稿日期:2018-05-14基金项目:国家自然科学基金项目(11402117); 中国博士后科学基金项目(2013M541676)作者简介:陈升富(1993- ),男,硕士研究生,研究方向为弹箭飞行制导与控制。E-mail:chenshengfu@njust.edu.cn。通讯作者:常思江(1983- ),男,副研究员,博士,研究方向为外弹道设计理论、弹箭飞行控制技术。E-mail:ballistics@126.com。
更新日期/Last Update: 2018-12-30