Major mission of Saturn is to serve as launch vehicle for Apollo lunar landing; based on D.F.Lawden's equation, semi-explicit, "iterative" Saturn guidance equations are derived; they were successfully flight tested on Saturn I and analyzed for main Apollo mission and other applications; Saturn guidance hardware; stability and error analysis.
Iterative guidance law for Saturn
IEEE -- Tech Paper
12th IEEE -- East Coast Conference on Aerospace and Navigational Electronics Meeting ; 1965 Control
IEEE Technical Papers ; n 3.4.1
1965
13 pages
Conference paper
English
© Metadata Copyright Elsevier B. V. All rights reserved.