OPTIMAL GUIDANCE FOR AERODYNAMICALLY CONTROLLED REENTRY VEHICLES

被引:8
作者
DEVIRGIL.MA
WELLS, GR
SCHIRING, EE
机构
[1] AEROSP CORP,TECH STAFF,GUID & CONTROL DIV,EL SEGUNDO,CA 90245
[2] LOGICON INC,TECH STAFF,SYST ANAL DEPT,SAN PEDRO,CA
关键词
D O I
10.2514/3.49485
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:1331 / 1337
页数:7
相关论文
共 8 条
[1]  
Anderson B.D.O., 1971, LINEAR OPTIMAL CONTR
[2]  
BRYSON A, 1969, APPLIED OPTIMAL CONT
[3]  
DUIVEN EM, 1969, 254820100020 BOEING
[4]  
GLOVER LA, 1971, TG1164 JOHNS HOPK U
[5]  
HOFFMAN WC, 1970, J SPACECRAFT ROCKETS, V7, P196
[6]  
KOVATCH G, 1964, 9 T S BALL MISS SPAC, V1, P327
[7]  
Kwakernaak H., 1972, LINEAR OPTIMAL CONTR
[8]  
WHITE JS, 1971, X2417 NASA TM