Three-Dimensional Nonlinear Impact Time Guidance Using Predicted Interception Point

被引：5
|
作者：
Sinha, Abhinav [1 ]
Nanavati, Rohit V. [2 ]
Ranjan Kumar, Shashi [3 ]
机构：
[1] Univ Texas San Antonio, Dept Elect & Comp Engn, Unmanned Syst Lab, San Antonio, TX 78249 USA
[2] Loughborough Univ, Ctr Autonomous Syst, Dept Aeronaut & Automot Engn, Loughborough LE11 3TU, England
[3] Indian Inst Technol, Dept Aerosp Engn, Intelligent Syst & Control Lab, Mumbai 400076, India
来源：
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS | 2023年 / 46卷 / 03期
关键词：
LAW; ANGLE; MISSILES; ATTACK;
D O I：
10.2514/1.G007122
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：608 / 617
页数：10
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