GUIDANCE LAWS FOR SHORT-RANGE TACTICAL MISSILES

被引:61
作者
PASTRICK, HL
SELTZER, SM
WARREN, ME
机构
[1] CONTROL DYNAM CO,HUNTSVILLE,AL
[2] SYST DYNAM INC,GAINESVILLE,FL
来源
JOURNAL OF GUIDANCE AND CONTROL | 1981年 / 4卷 / 02期
关键词
D O I
10.2514/3.56060
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:98 / 108
页数:11
相关论文
共 112 条
[1]  
ABZUG MJ, 1967, J SPACECRAFT ROC FEB, P279
[2]  
ABZUG MJ, 1979, J GUIDANCE CONTR MAY, P253
[3]  
ACUS RW, 1972, LS52 AGARD REPT
[4]   MISSILE GUIDANCE BY 3-DIMENSIONAL PROPORTIONAL NAVIGATION [J].
ADLER, FP .
JOURNAL OF APPLIED PHYSICS, 1956, 27 (05) :500-507
[5]   A Near-Optimal Closed-Loop Solution Method for Nonsingular Zero-Sum Differential Games [J].
Anderson, G. M. .
JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS, 1974, 13 (03) :303-318
[6]  
ANDREW GM, 1970, J SPACECRAFT ROC DEC, P59
[7]  
ANDRUS JF, 1970, AIAA J DEC, P2252
[8]  
ARBENZ K, 1970, IEEE T AERO ELEC SYS, P455
[9]  
ASHER RB, 1974, P JOINT AUTOMATIC CO, P4
[10]  
ASHER RB, 1974, J SPACECRAFT ROC MAR, P204