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STABILITY OF A DUAL-SPIN SPACECRAFT WITH A FLEXIBLE MOMENTUM WHEEL
被引:8
作者
:
BAINUM, PM
论文数:
0
引用数:
0
h-index:
0
BAINUM, PM
FUECHSEL, PG
论文数:
0
引用数:
0
h-index:
0
FUECHSEL, PG
FEDOR, JV
论文数:
0
引用数:
0
h-index:
0
FEDOR, JV
机构
:
来源
:
JOURNAL OF SPACECRAFT AND ROCKETS
|
1972年
/ 9卷
/ 09期
关键词
:
D O I
:
10.2514/3.61768
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:640 / &
相关论文
共 9 条
[1]
MOTION AND STABILITY OF A DUAL-SPIN SATELLITE WITH NUTATION DAMPING
BAINUM, PM
论文数:
0
引用数:
0
h-index:
0
BAINUM, PM
FUECHSEL, PG
论文数:
0
引用数:
0
h-index:
0
FUECHSEL, PG
MACKISON, DL
论文数:
0
引用数:
0
h-index:
0
MACKISON, DL
[J].
JOURNAL OF SPACECRAFT AND ROCKETS,
1970,
7
(06)
: 690
-
&
[2]
BAINUM PM, 1969, TG1072 JOHNS HOPK U
[3]
FLATLEY TW, 1971, TRR362 NASA
[4]
ATTITUDE STABILITY CRITERIA FOR DUAL SPIN SPACECRAFT
LIKINS, PW
论文数:
0
引用数:
0
h-index:
0
LIKINS, PW
[J].
JOURNAL OF SPACECRAFT AND ROCKETS,
1967,
4
(12)
: 1638
-
&
[5]
STABLE LIMIT CYCLES DUE TO NONLINEAR DAMPING IN DUAL-SPIN SPACECRAFT
LIKINS, PW
论文数:
0
引用数:
0
h-index:
0
LIKINS, PW
TSENG, GT
论文数:
0
引用数:
0
h-index:
0
TSENG, GT
MINGORI, DL
论文数:
0
引用数:
0
h-index:
0
MINGORI, DL
[J].
JOURNAL OF SPACECRAFT AND ROCKETS,
1971,
8
(06)
: 568
-
&
[6]
EFFECTS OF ENERGY DISSIPATION ON ATTITUDE STABILITY OF DUAL-SPIN SATELLITES
MINGORI, DL
论文数:
0
引用数:
0
h-index:
0
机构:
Aerospace Corporation, Control Systems Department, El Segundo, CA
MINGORI, DL
[J].
AIAA JOURNAL,
1969,
7
(01)
: 20
-
&
[7]
SEN AK, 1970, NASA204 GODD SPAC FL
[8]
VARIABLE PARAMETER NUTATION DAMPER FOR SAS-A
TOSSMAN, BE
论文数:
0
引用数:
0
h-index:
0
TOSSMAN, BE
[J].
JOURNAL OF SPACECRAFT AND ROCKETS,
1971,
8
(07)
: 743
-
&
[9]
WHITTAKER ET, 1959, TREATISE ANALYTICAL, P41
←
1
→
共 9 条
[1]
MOTION AND STABILITY OF A DUAL-SPIN SATELLITE WITH NUTATION DAMPING
BAINUM, PM
论文数:
0
引用数:
0
h-index:
0
BAINUM, PM
FUECHSEL, PG
论文数:
0
引用数:
0
h-index:
0
FUECHSEL, PG
MACKISON, DL
论文数:
0
引用数:
0
h-index:
0
MACKISON, DL
[J].
JOURNAL OF SPACECRAFT AND ROCKETS,
1970,
7
(06)
: 690
-
&
[2]
BAINUM PM, 1969, TG1072 JOHNS HOPK U
[3]
FLATLEY TW, 1971, TRR362 NASA
[4]
ATTITUDE STABILITY CRITERIA FOR DUAL SPIN SPACECRAFT
LIKINS, PW
论文数:
0
引用数:
0
h-index:
0
LIKINS, PW
[J].
JOURNAL OF SPACECRAFT AND ROCKETS,
1967,
4
(12)
: 1638
-
&
[5]
STABLE LIMIT CYCLES DUE TO NONLINEAR DAMPING IN DUAL-SPIN SPACECRAFT
LIKINS, PW
论文数:
0
引用数:
0
h-index:
0
LIKINS, PW
TSENG, GT
论文数:
0
引用数:
0
h-index:
0
TSENG, GT
MINGORI, DL
论文数:
0
引用数:
0
h-index:
0
MINGORI, DL
[J].
JOURNAL OF SPACECRAFT AND ROCKETS,
1971,
8
(06)
: 568
-
&
[6]
EFFECTS OF ENERGY DISSIPATION ON ATTITUDE STABILITY OF DUAL-SPIN SATELLITES
MINGORI, DL
论文数:
0
引用数:
0
h-index:
0
机构:
Aerospace Corporation, Control Systems Department, El Segundo, CA
MINGORI, DL
[J].
AIAA JOURNAL,
1969,
7
(01)
: 20
-
&
[7]
SEN AK, 1970, NASA204 GODD SPAC FL
[8]
VARIABLE PARAMETER NUTATION DAMPER FOR SAS-A
TOSSMAN, BE
论文数:
0
引用数:
0
h-index:
0
TOSSMAN, BE
[J].
JOURNAL OF SPACECRAFT AND ROCKETS,
1971,
8
(07)
: 743
-
&
[9]
WHITTAKER ET, 1959, TREATISE ANALYTICAL, P41
←
1
→