STOCHASTIC RESPONSE ANALYSIS, ORDER REDUCTION, AND OUTPUT-FEEDBACK CONTROLLERS FOR FLEXIBLE SPACECRAFT

被引:3
作者
HABLANI, HB [1 ]
机构
[1] NASA,LYNDON B JOHNSON SPACE CTR,NRC,HOUSTON,TX 77058
关键词
D O I
10.2514/3.19940
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:94 / 103
页数:10
相关论文
共 23 条
[1]  
ARMSTRONG ES, 1972, NASA1106 LANGL RES C
[2]   CONTROL LOGIC FOR PARAMETER INSENSITIVITY AND DISTURBANCE ATTENUATION [J].
ASHKENAZI, A ;
BRYSON, AE .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1982, 5 (04) :383-388
[3]  
BENDAT JS, 1980, ENG APPLICATIONS COR, P115
[4]  
CRANDALL SH, 1971, JUN P S DYN RESP STR, P55
[5]   MULTIVARIABLE FEEDBACK DESIGN - CONCEPTS FOR A CLASSICAL-MODERN SYNTHESIS [J].
DOYLE, JC ;
STEIN, G .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1981, 26 (01) :4-16
[6]   WIDEBAND RANDOM AXISYMMETRIC VIBRATION OF CYLINDRICAL-SHELLS [J].
ELISHAKOFF, I ;
ZANTEN, ATV ;
CRANDALL, SH .
JOURNAL OF APPLIED MECHANICS-TRANSACTIONS OF THE ASME, 1979, 46 (02) :417-422
[7]   DYNAMICS AND CONTROL OF A DEFORMABLE GYROSTAT, UTILIZING CONTINUUM VEHICLE MODES [J].
HABLANI, HB .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1983, 6 (06) :499-510
[8]  
HABLANI HB, 1982, AUG P AIAA GUID CONT, P597
[9]   EXTENSIONS OF SUBOPTIMAL OUTPUT-FEEDBACK CONTROL WITH APPLICATION TO LARGE SPACE STRUCTURES [J].
HEGG, DR .
JOURNAL OF GUIDANCE AND CONTROL, 1981, 4 (06) :637-641
[10]  
HILDEBRAND FB, 1976, ADV CALCULUS APPLICA, P539