ROBUST TIME-OPTIMAL CONTROL - FREQUENCY-DOMAIN APPROACH

被引:125
作者
SINGH, T [1 ]
VADALI, SR [1 ]
机构
[1] TEXAS A&M UNIV, COLLEGE STN, TX 77843 USA
关键词
D O I
10.2514/3.21204
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The design of nonrobust and robust time-optimal controllers for linear systems in the frequency domain is presented. The bang-bang profile is represented as the superposition of time-delayed step inputs or the output of a time-delay filter subject to a step input. A parameter optimization problem is formulated to minimize the final time of the maneuver with the constraint that the time-delay filter cancels all of the poles of the system. The issue of robustness to errors in the model is addressed by placing multiple zeros of the time-delay filter at the estimated locations of the poles of the system. The design technique is illustrated on representative models of large space structures, for rest-to-rest, time-optimal, and robust time-optimal maneuvers. Spin-up maneuvers are shown to be special cases of the general formulation.
引用
收藏
页码:346 / 353
页数:8
相关论文
共 14 条
[1]   TIME-OPTIMAL SLEWING OF FLEXIBLE SPACECRAFT [J].
BENASHER, J ;
BURNS, JA ;
CLIFF, EM .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1992, 15 (02) :360-367
[2]  
GRACE A, MATLAB OPTIMIZATION
[3]  
HABLANI HB, 1991, P AIAA GUID NAV CONT, V1, P488
[4]  
HERMES H., 1969, MATH SCI ENG
[5]   NEAR-MINIMUM-TIME CONTROL OF DISTRIBUTED PARAMETER-SYSTEMS - ANALYTICAL AND EXPERIMENTAL RESULTS [J].
JUNKINS, JL ;
RAHMAN, ZH ;
BANG, H .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1991, 14 (02) :406-415
[6]  
LIU Q, 1991, P AIAA GUID NAV CONT, V1, P443
[7]  
RAJAN N, 1987, P AIAA GUIDANCE NAVI, P1222
[8]  
SCRIVENER S, 1992, FEB AIAA SPAC MECH M
[9]   PRESHAPING COMMAND INPUTS TO REDUCE SYSTEM VIBRATION [J].
SINGER, NC ;
SEERING, WP .
JOURNAL OF DYNAMIC SYSTEMS MEASUREMENT AND CONTROL-TRANSACTIONS OF THE ASME, 1990, 112 (01) :76-82
[10]  
SINGH G, 1990, J ASTRONAUT SCI, V38, P41