DocumentCode
2592266
Title
A design algorithm using Z-plane closed loop pole placement
Author
Gatlin, James A.
Author_Institution
NASA Goddard Space Flight Center, Greenbelt, MD, USA
fYear
1990
fDate
15-18 Oct 1990
Firstpage
64
Lastpage
69
Abstract
It is argued that the design of a single input single output (SISO) control system is simplified if the designer has direct control over the closed loop poles. A space-laser-communications design example utilizing a two-transform algorithm that constructs a generic discrete compensator is presented. The plant in the example has an anti-aliasing filter, a double integrator, a torquer time constant, and a sample-and-hold as continuous elements, and a discrete proportional plus integral module. This fifth-order system is representative of many instrument pointing control systems. Poles resulting from the compensator are placed near the origin of the Z-plane so that the response is dominated by the closed loop poles from the plant. Root locus, time response, and frequency response data are given. Normalization by the sample interval is used to provide a dimensionless example
Keywords
Z transforms; closed loop systems; control system synthesis; optical links; poles and zeros; space communication links; Z-plane; Z-plane closed loop pole placement; anti-aliasing filter; design algorithm; discrete proportional plus integral module; double integrator; fifth-order system; frequency response; generic discrete compensator; root locus; sample-and-hold; single input single output control; space-laser-communications; time response; torquer time constant; two-transform algorithm; Algorithm design and analysis; Control system synthesis; Control systems; Filters; Frequency response; Instruments; NASA; State feedback; Time factors; Transfer functions;
fLanguage
English
Publisher
ieee
Conference_Titel
Digital Avionics Systems Conference, 1990. Proceedings., IEEE/AIAA/NASA 9th
Conference_Location
Virginia Beach, VA
Type
conf
DOI
10.1109/DASC.1990.111263
Filename
111263
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