Sub-optimal analytic guidance for reusable launch vehicles
"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.
Mechanical and Aerospace Engineering
M.S. in Aerospace Engineering
University of Missouri--Rolla
x, 60 leaves
© 2003 Katie Amanda Grantham, All rights reserved.
Thesis - Citation
Library of Congress Subject Headings
Guidance systems (Flight) -- Design
Space vehicles -- Guidance systems
Print OCLC #
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
Grantham, Katie, "Sub-optimal analytic guidance for reusable launch vehicles" (2003). Masters Theses. 2384.