Trajectory-shaping guidance for interception of ballistic missiles during the boost phase

被引:17
作者
Lukacs, John A., IV [1 ]
Yakimenko, Oleg A. [2 ]
机构
[1] USA, Def Tech Informat Ctr, Ft Belvoir, VA 22060 USA
[2] USN, Postgrad Sch, Dept Mech & Astronaut Engn, Monterey, CA 93943 USA
关键词
D O I
10.2514/1.32262
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:1524 / 1531
页数:8
相关论文
共 11 条
[1]  
[Anonymous], EXPERIENCE EMPLOYING
[2]  
Barton D K, 2004, REV MODERN PHYS, V76, p[1, 301]
[3]  
CORNELL C, SHIELDING AM NATL MI
[4]  
Dobrokhodov VN, 1999, J COMPUT SYS SC INT+, V38, P262
[5]  
John IV A.Lukacs, 2007, AIAA GUID NAV CONTR
[6]  
Kaminer I., 2007, AIAA GUID NAV CONTR
[7]  
*MISS DEF AG, MISS DEF WORLDW
[8]  
YAKIMENKO O, 2006, CONTR 2006 C UK AUT
[9]   Direct method for rapid prototyping of near-optimal aircraft trajectories [J].
Yakimenko, OA .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 2000, 23 (05) :865-875
[10]  
Yakimenko OA, 2008, AIAA GUID NAV CONTR