MANEUVER AND VIBRATION CONTROL OF HYBRID COORDINATE SYSTEMS USING LYAPUNOV STABILITY THEORY

被引:36
作者
JUNKINS, JL
BANG, HC
机构
[1] Department of Aerospace Engineering, Texas A and M University, College Station, TX
[2] Department of Aeronautics and Astronautics, Naval Postgraduate School, Monterey, CA
关键词
D O I
10.2514/3.21066
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
In this study, we present a generalized control law design methodology that covers a large class of systems, especially flexible structures described by hybrid discrete/distributed coordinate systems. The Lyapunov stability theory is used to develop globally stabilizing control laws. A hybrid version of Hamilton's canonical equations is introduced, which provides a direct path to designing stabilizing control laws for general nonlinear hybrid systems. The usual loss of robustness due to model reduction is overcome by this Lyaponov approach, which does not require truncation of the flexible systems into finite dimensional discrete systems.
引用
收藏
页码:668 / 676
页数:9
相关论文
共 22 条
[2]   FEEDBACK-CONTROL OF FLEXIBLE SYSTEMS [J].
BALAS, MJ .
IEEE TRANSACTIONS ON AUTOMATIC CONTROL, 1978, 23 (04) :673-679
[3]  
BANG H, 1991, AAS91143 PAP
[4]  
BREAKWELL J, 1981, J GUIDANCE CONTROL, V4, P427
[5]  
Craig RR., 1981, STRUCT DYNAM-US
[6]   MISSION-FUNCTION CONTROL FOR SLEW MANEUVER OF A FLEXIBLE SPACE STRUCTURE [J].
FUJII, H ;
ISHIJIMA, S .
JOURNAL OF GUIDANCE CONTROL AND DYNAMICS, 1989, 12 (06) :858-865
[7]  
Goldstein H., 1980, CLASSICAL MECH, V2nd ed
[8]  
HAILEY JA, 1992, AIAA GUIDANCE NAVIGA
[9]  
JUNKINS J, 1989, 7TH P VPI SU S DYN C
[10]   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