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  5. Tightly coupled GPS-gyro integration for spacecraft attitude determination

Tightly coupled GPS-gyro integration for spacecraft attitude determination

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Author(s)
Puri, Varun
Advisor(s)
John J. Deyst, Jr.
Date Issued
1997
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1997.
Includes bibliographical references (p. 197-199).
Subjects
Aeronautics and Astronautics
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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http://dspace.mit.edu/handle/1721.1/7582
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http://hdl.handle.net/1721.1/50315
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