Intercept Mode Suitable for the Space-Based Kinetic Energy Interceptor

被引：0

作者：

端军红 ^{[1
,2
]}

刘跃峰 ^{[2
]}

万开方 ^{[3
]}

机构：

[1] Air and Missile Defense College, Air Force Engineering University

[2] Science and Technology on Electro-Optic Control Laboratory

[3] School of Electronics and Information,Northwestern Polytechnical University

来源：

Journal of Shanghai Jiaotong University(Science) | 2019年 / 24卷 / 05期

基金：

中国国家自然科学基金;

关键词：

kinetic energy interceptor(KEI); intercept mode; trajectory planning; guidance law; pregnable area;

D O I：

暂无

中图分类号：

V423 [航天器构造和设计]; TJ86 [航天武器];

学科分类号：

082501 ; 082601 ; 1111 ;

摘要：

The intercept mode of space-based kinetic energy interceptor（KEI） is an essential problem to be solved in the concept design of KEI and is closely related to the KEI’s detailed designing and practical applications.However, this problem has not yet been investigated systematically and comprehensively. A suitable intercept mode for the KEI is proposed in this research. The intercept mode consists of three basic elements: the specific operation procedure, general scheme for the intercept trajectory, and mathematical model of the intercept mode.Numerical example is provided to demonstrate the feasibility and effectiveness of the intercept mode. The intercept mode proposed in this research is capable of achieving a rapid intercept, and is applicable to the universal space interception.

引用

页码：671 / 680

页数：10

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