Two high-authority control/low-authority control algorithms are presented and experimentally validated on a fast slewing beam system. The first one termed the constrained motion method in two-stage (CMM-TS) accomplishes the rigid-body motion control and the optimal control of vibration suppression by a stepping motor. Another termed the constrained motion method in combination (CMM-CO) combines both the optimal control from stepping motor and active damping control from piezoelectric actuator for vibration suppression. Experimental results show that these algorithms are concise in formulation, efficient in hardware realization, and effective in vibration suppression.
1.
Das, A., “Large Angle Maneuver Experiments in Ground-Based Laboratories,” AlAA paper, Vol. AIAA-90-1236-CP.
2.
Fujii
H.
Ohtsuka
T.
Udou
S.
Mission Function Control for a Slew Maneuver Experiment
,” J. of Guidance
, Vol. 14
, No. 5
, 1991
, pp. 986
–992
, Sept–Oct.3.
Juang
J. N.
Turner
J. D.
Chun
H. M.
Closed-Form Solution for a Class of Optimal Quadratic Regulator Problems with Terminal Constraints
,” ASME JOURNAL OF DYNAMIC SYSTEMS, MEASUREMENT, AND CONTROL
, Vol. 108
, Mar. 1986
, pp. 44
–48
.4.
Juang
J. N.
Horta
L. G.
Robertshaw
H. H.
A Slewing Control Experiment for Flexible Structures
,” J. of Guidance
, Vol. 9
, No. 5
, Sept.–Oct. 1986
, pp. 599
–607
.5.
Junkins, J. L., and Turner, J. D., Optimal Spacecraft Rotational Maneuvers, Elsevier Science Publishing Company New York, 1986.
6.
Junkins
J. L.
Rahman
Z. H.
Bang
H.
Near-Minimum-time Control of Distributed Parameter System: Analytical and Experimental Results
,” J. of Guidance
, Vol. 14
, No. 2
, Mar.–Apr. 1991
, pp. 406
–415
.7.
Liu
Y. C.
Yang
S. M.
Three Simple and Efficient Methods for Vibration Control of Slewing Flexible Structures
,” ASME JOURNAL OF DYNAMIC SYSTEMS, MEASUREMENT, AND CONTROL
, Vol. 115
, No. 4
, 1993
, pp. 725
–730
.8.
Murotsu
Y.
Okubo
H.
Terui
F.
Low-Authority Control of Large Space Structures by Using a Tendon Control System
,” J. of Guidance
, Vol. 12
, No. 2
, Mar.–Apr. 1989
, pp. 264
–272
.9.
Singh
G.
Kabamba
P. T.
McClamroch
N. H.
Planar, Time-Optimal, Rest-to-Rest Slewing Maneuvers of Flexible Spacecraft
,” J. of Guidance
, Vol. 12
, No. 1
, Jan.–Feb. 1989
, pp. 71
–81
.10.
Yang
S. M.
Modal Analysis of Structures with Holonomic Constraints
,” AIAA Journal
, Vol. 30
, No. 10
, Oct. 1992
, pp. 2526
–2531
.
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