An integrated design, control, and trajectory optimization algorithm for future planetary (Martian) entry/lander vehicles
Name
29425223-MIT.pdf
Description
Full printable version
Size
7.48 MB
Format
Adobe PDF
Checksum (MD5)
57448ac695384f791e446d4e7244b499
Author(s)
Bratkovich, Thomas E. (Thomas Edward)
Advisor(s)
Joseph F. Shea.
Date Issued
1993
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1993.
Includes bibliographical references (p. 221-226).
Subjects
Aeronautics and Astronautics
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
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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.
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