An extended analytic range corrector method for the space shuttle entry guidance algorithm

Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, 2018. === Cataloged from PDF version of thesis. === Includes bibliographical references (pages 99-101). === Space shuttle entry guidance with an extended analytic range corrector method is presented. The...

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Bibliographic Details
Main Author: Evans, Erin Elizabeth
Other Authors: Jonathan P. How and Stephen Thrasher.
Format: Others
Language:English
Published: Massachusetts Institute of Technology 2018
Subjects:
Online Access:http://hdl.handle.net/1721.1/119296