Masters Theses
Abstract
"This thesis shows that reaction jet thrust pulses, each of constant amplitude and time duration, in conjunction with sampled data error information can provide satisfactory position and/or attitude control for space vehicles.
Incremental phase-plane analysis of the system yields a technique for determining system response and suggests a means of compensation. Control system response for the vehicle under the influence of external forces is shown to be satisfactory by digital computer simulation"--Abstract, page ii.
Advisor(s)
Noack, Thomas L.
Committee Member(s)
Brown, Harry A., 1925-1995
Chenoweth, Robert D.
Pagano, Sylvester J., 1924-2006
Department(s)
Electrical and Computer Engineering
Degree Name
M.S. in Electrical Engineering
Publisher
University of Missouri at Rolla
Publication Date
1966
Pagination
viii, 69 pages
Note about bibliography
Includes bibliographical references (pages 67-68)
Rights
© 1966 John D. Corrigan, All rights reserved.
Document Type
Thesis - Open Access
File Type
text
Language
English
Subject Headings
Feedback control systems -- Design -- Computer simulation
Adaptive control systems
Feedback control systems -- Mathematical models
Thesis Number
T 1893
Print OCLC #
5976101
Electronic OCLC #
897205179
Link to Catalog Record
Recommended Citation
Corrigan, John D., "A nonlinear sampled data feedback control system employing pulsed thrust position control" (1966). Masters Theses. 5764.
https://scholarsmine.mst.edu/masters_theses/5764
