DocumentCode
1450371
Title
Optimal root loci of flexible space structures
Author
Williams, Trevor
Author_Institution
Dept. of Aerosp. Eng. & Eng. Mech., Cincinnati Univ., OH, USA
Volume
36
Issue
3
fYear
1991
fDate
3/1/1991 12:00:00 AM
Firstpage
375
Lastpage
377
Abstract
It is shown that simple generic properties can be proved for the optimal root loci of flexible space structures (FSS). It is proved that the angles and rates at which closed-loop poles depart from the open-loop poles can be found by inspection for any FSS with sufficiently widely space natural frequencies. Similar results also apply to the angles at which certain loci approach the transmission zeros of any FSS with compatible (physically colocated and coaxial) sensors and actuators, as a consequence of the special properties of the zeros of such systems. Finally, determining the number and orders of the Butterworth configurations of such as FSS is much more straightforward than for a general state-space system: it amounts only to checking whether structural displacements or their rates are the measured outputs. These results depend on the fundamental second-order nature of such systems, and five considerably more insight than is possible a priori for general linear multivariable systems
Keywords
aerospace control; large-scale systems; poles and zeros; root loci; Butterworth configurations; closed-loop poles; flexible space structures; open-loop poles; optimal root loci; structural displacements; transmission zeros; Aerodynamics; Control systems; Cost function; Frequency selective surfaces; H infinity control; MIMO; Mirrors; Optimal control; Poles and zeros; Regulators;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/9.73575
Filename
73575
Link To Document