PARAMETER PLANE ANALYSIS FOR LARGE FLEXIBLE SPACECRAFT

被引：2

作者：

ASNER, BA ^{[1
]}

SELTZER, SM ^{[1
]}

机构：

[1] CONTROL DYNAM CO,HUNTSVILLE,AL 35804

来源：

JOURNAL OF GUIDANCE AND CONTROL | 1981年 / 4卷 / 03期

关键词：

D O I：

10.2514/3.56080

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：284 / 290

页数：7

共 19 条

[1] ASNER B, 1973, J SPACECRAFT ROCKETS, V10, P200
[2] ON PARAMETER STABILITY REGIONS FOR SEVERAL PARAMETERS USING FREQUENCY RESPONSE
GEORGE, JH
[J]. IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1967, AC12 (02) : 197 - &
[3] HAEUSSERMANN W, 1957, JET PROPULSION JUL, P787
[4] HUANG JT, 1970, AUG AIAA GUID CONTR
[5] Neimark Y. I., 1949, APPL MATH MECH-ENGL, V13, P349
[6] Seltzer S. M., 1978, Journal of Guidance and Control, V1, P427, DOI 10.2514/3.21068
[7] Seltzer S. M., 1975, Computers & Electrical Engineering, V2, P35, DOI 10.1016/0045-7906(75)90031-2
[8] SATELLITE DIGITAL CONTROLLER
SELTZER, SM
[J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1977, 14 (08) : 509 - 511
[9] LARGE SPACE TELESCOPE OSCILLATIONS INDUCED BY CMG FRICTION
SELTZER, SM
[J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1975, 12 (02) : 96 - 105
[10] AN ACCELERATION VECTOR ATTITUDE CONTROL SYSTEM
SELTZER, SM
[J]. JOURNAL OF SPACECRAFT AND ROCKETS, 1968, 5 (06) : 666 - &