DocumentCode
3278926
Title
Flatness-based guidance for planetary landing
Author
Desiderio, D. ; Lovera, M.
Author_Institution
Dipt. di Elettron. e Inf., Politec. di Milano, Milan, Italy
fYear
2010
fDate
June 30 2010-July 2 2010
Firstpage
3642
Lastpage
3647
Abstract
The problem of guidance law design for planetary landing is considered and an approach based on the flatness property of the descent equations is proposed. Analytical solutions and numerical schemes based on polynomial and pseudo-spectral approximations for the problem are considered and compared in a simulation study.
Keywords
aircraft landing guidance; control system synthesis; polynomial approximation; descent equation; flatness-based guidance; guidance law design; planetary landing; polynomial approximation; pseudo-spectral approximation; Analytical models; Computational modeling; Control systems; Equations; Mars; Mobile robots; Moon; Navigation; Polynomials; Remotely operated vehicles;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference (ACC), 2010
Conference_Location
Baltimore, MD
ISSN
0743-1619
Print_ISBN
978-1-4244-7426-4
Type
conf
DOI
10.1109/ACC.2010.5530626
Filename
5530626
Link To Document