Repository logo
Log in(current)
Repository logoMIT Open ScholarshipDSpace@MIT
  1. Home
  2. MIT Libraries
  3. MIT Theses
  4. Graduate Theses
  5. An optimal approach to computer control of a highly coupled satellite attitude loop

An optimal approach to computer control of a highly coupled satellite attitude loop

Thumbnail Image
Download
Name

11117288-MIT.pdf

Description
Full printable version
Size

6.21 MB

Format

Adobe PDF

Checksum (MD5)

3479ada087811d84964feed2a32c4783

Author(s)
McCasland, William Neil
Advisor(s)
Richard H. Battin.
Date Issued
1981
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1981.
Microfiche copy available in Archives and Barker
Bibliography: leaves 108-109.
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
M.I.T. theses are protected by
copyright. They may be viewed from this source for any purpose, but
reproduction or distribution in any format is prohibited without written
permission. See provided URL for inquiries about permission.
http://dspace.mit.edu/handle/1721.1/7582
Persistent DSpace Link
http://hdl.handle.net/1721.1/49887
Repository logo
PrivacyPermissionsAccessibilityContact us
Repository logo
Notify us about copyright concerns.