DocumentCode :
2164757
Title :
State estimation by interval analysis for a nonlinear differential aerospace model
Author :
Ribot, Pauline ; Jauberthie, Carine ; Trave-Massuyes, Louise
Author_Institution :
LAAS, Univ. of Toulouse, Toulouse, France
fYear :
2007
fDate :
2-5 July 2007
Firstpage :
4839
Lastpage :
4844
Abstract :
This paper deals with guaranteed state estimation in a bounded-error context for an aerospace model. Perturbations are assumed bounded but otherwise unknown. The main tools to solve this problem are the guaranteed techniques for ordinary differential equation integration and set inversion. The obtained results show the efficiency of the method.
Keywords :
aerospace control; differential equations; nonlinear dynamical systems; set theory; state estimation; bounded-error context; interval analysis; nonlinear differential aerospace model; nonlinear dynamic system; ordinary differential equation integration; set inversion; state estimation; Algorithm design and analysis; Differential equations; Mathematical model; Noise; Prediction algorithms; State estimation; Vectors; Bounded noise; Continuous-time systems; Interval analysis; Nonlinear systems; State estimation;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (ECC), 2007 European
Conference_Location :
Kos
Print_ISBN :
978-3-9524173-8-6
Type :
conf
Filename :
7068689
Link To Document :
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