Please use this identifier to cite or link to this item:
https://hdl.handle.net/2440/28773
Type: | Conference paper |
Title: | Performance of a predictive guidance system for booster flyback |
Author: | Tetlow, M. Schottle, U. Evans, M. Schneider, G. |
Citation: | The proceedings of the 5th Asian Control Conference : Melbourne, 20-23 July, 2004, Vol. 2, pp.745-753 |
Publisher: | IEEE |
Publisher Place: | CD-ROM |
Issue Date: | 2004 |
ISBN: | 0734030169 |
Conference Name: | Asian Control Conference (5th : 2004 : Melbourne, Australia) |
Editor: | Evans, R. Mareels, I. |
Statement of Responsibility: | M.R. Tetlow, U.M. Schottle, M.E. Evans and G.M. Schneider |
Abstract: | The aim of this study is to develop and test a robust guidance strategy for use on the flyback mission of a winged launch booster. The guidance system employs a numerical Newton-Raphson restoration technique to update steering parameters, coupled with heuristic logic, to improve robustness. The guidance system uses a prediction of the final state of the launch vehicle to close the feedback loop and is therefore called "predictive guidance". |
Description (link): | http://ieeexplore.ieee.org/xpl/freeabs_all.jsp?arnumber=1426744 |
Appears in Collections: | Aurora harvest 2 Mechanical Engineering conference papers |
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