SOME SPECIAL CASES OF SPIN-YAW LOCK-IN

被引:34
作者
MURPHY, CH
机构
关键词
D O I
10.2514/3.20480
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:771 / 776
页数:6
相关论文
共 24 条
[1]   A METHOD OF DETERMINING SOME AERODYNAMIC COEFFICIENTS FROM SUPERSONIC FREE-FLIGHT TESTS OF A ROLLING MISSILE [J].
BOLZ, RE ;
NICOLAIDES, JD .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (10) :609-621
[2]  
BOLZ RE, 1949, AD801752
[5]  
Maple C.G., 1949, Q APPL MATH, V4, P345
[7]   NONLINEAR LIMIT MOTIONS OF A SLIGHTLY ASYMMETRIC REENTRY VEHICLE [J].
MURPHY, CH ;
BRADLEY, JW .
AIAA JOURNAL, 1975, 13 (07) :851-857
[8]   RESPONSE OF AN ASYMMETRIC MISSILE TO SPIN VARYING THROUGH RESONANCE [J].
MURPHY, CH .
AIAA JOURNAL, 1971, 9 (11) :2197-&
[9]  
MURPHY CH, 1975, ADA005165
[10]  
MURPHY CH, 1979, J GUIDANCE CONTROL, V4, P504