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
Link To Document :
بازگشت