Masters Theses

Title

Sub-optimal analytic guidance for reusable launch vehicles

Abstract

"This thesis presents a guidance scheme for the Terminal Area Energy Management (TAEM) and Approach and Landing phases of flight for the next generation of reusable launch vehicles (RLVs). The guidance scheme presented is developed in two parts, the kappa guidance section and the touchdown trajectory section."--Abstract, page iii.

Department(s)

Mechanical and Aerospace Engineering

Degree Name

M.S. in Aerospace Engineering

Publisher

University of Missouri--Rolla

Publication Date

Fall 2003

Pagination

x, 60 leaves

Rights

© 2003 Katie Amanda Grantham, All rights reserved.

Document Type

Thesis - Citation

File Type

text

Language

English

Library of Congress Subject Headings

Guidance systems (Flight) -- Design
Space vehicles -- Guidance systems

Thesis Number

T 8308

Print OCLC #

54853656

Link to Catalog Record

Full-text not available: Request this publication directly from Missouri S&T Library or contact your local library.

http://laurel.lso.missouri.edu/record=b5072223~S5

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