Analysis and error model for a two-degrees-of-freedom elastically supported tuned gyro.

Graham, David Bruce

Analysis and error model for a two-degrees-of-freedom elastically supported tuned gyro.

Download

Name

29060720-MIT.pdf

Description

Full printable version

Size

2.27 MB

Format

Adobe PDF

Checksum (MD5)

5be7e55ebe6a5f29de0fa0bbd532d816

Author(s)

Graham, David Bruce

Advisor(s)

Walter Wrigley.

Date Issued

1972

Publisher

Massachusetts Institute of Technology

Description

Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1972.

Includes bibliographical references.

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/1721.1/29863