Algebraic solution of differential geometric guidance command and time delay control

被引:29
作者
Li KeBo [1 ]
Chen Lei [1 ]
Tang GuoJin [1 ]
机构
[1] Natl Univ Def Technol, Coll Aerosp Sci & Engn, Changsha 410073, Hunan, Peoples R China
基金
中国国家自然科学基金;
关键词
differential geometric guidance command; explicit expression; time delay control; target acceleration estimation; PROPORTIONAL NAVIGATION; MISSILE GUIDANCE; INTERCEPTION; LAW;
D O I
10.1007/s11431-014-5730-y
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
According to the three-dimensional geometry of the engagement, the explicit algebraic expression of differential geometric guidance command (DGGC) is proposed. Compared with the existing solutions, the algebraic solution is much simpler and better for the further research of the characteristics of DGGC. Time delay control (TDC) is a useful method to tackle the uncertainty problem of a control system. Based on TDC, taking the target maneuvering acceleration as a disturbance, the estimation algorithm of the target maneuvering acceleration is presented, which can be introduced in DGGC to improve its performance. Then, the augmented DGGC (ADGGC) is obtained. The numerical simulation of intercepting a high maneuvering target is conducted to demonstrate the effectiveness of ADGGC.
引用
收藏
页码:565 / 573
页数:9
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