A discrete algorithm for following a desired model for systems that are non-linear or time varying is developed. The controller is developed with optimal control theory by finding the optimal control that would minimize a quadratic cost functional based on the error between the model and system for the previous sampling period. With this information a correction to the system command is formulated for the next sampling period. The stability of the algorithm is investigated and a stability criterion is found. Two examples are presented to show the characteristics of the controller. / Master of Science
Identifer | oai:union.ndltd.org:VTETD/oai:vtechworks.lib.vt.edu:10919/65031 |
Date | January 1973 |
Creators | Dunn, Henry Jackson |
Contributors | Aerospace Engineering |
Publisher | Virginia Polytechnic Institute and State University |
Source Sets | Virginia Tech Theses and Dissertation |
Language | English |
Detected Language | English |
Type | Thesis, Text |
Format | v, 40 leaves, application/pdf, application/pdf |
Rights | In Copyright, http://rightsstatements.org/vocab/InC/1.0/ |
Relation | OCLC# 34065657 |
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