A case study of two autopilot design methodologies : linear quadratic and H-infinity for a tail controlled missile
Name
28904478-MIT.pdf
Size
33.17 MB
Format
Adobe PDF
Checksum (MD5)
305313682c8b6d285abfb760b5470b07
Author(s)
Edeburn, Mark Anthony.
Advisor(s)
Michael Athans.
Date Issued
1993
Publisher
Massachusetts Institute of Technology
Description
Thesis: M.S., Massachusetts Institute of Technology, Department of Electrical Engineering and Computer Science, 1993
Includes bibliographical references.
Subjects
Electrical Engineering and Computer Science
MIT Department
Massachusetts Institute of Technology. Department of Electrical Engineering and Computer Science
Terms of Use
MIT theses may be protected by copyright. Please reuse MIT thesis content according to the MIT Libraries Permissions Policy, which is available through the URL provided.
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