DocumentCode :
596621
Title :
Self-regulation control scheme for reusable launch vehicle reentry attitude control
Author :
Jianshuang Song ; Zhang Ren ; Zhen Shen
Author_Institution :
Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
fYear :
2012
fDate :
18-20 Oct. 2012
Firstpage :
447
Lastpage :
451
Abstract :
Integrating sliding mode control and nonlinear dynamic inversion technique forms a new robust controller. Using nonlinear extended state observer to build the estimation of system disturbance, and based on the estimation, magnitude of the sliding mode item could be regulated to improve the control effect. Stability of This new controller is analyzed. This new control scheme is used in the reentry attitude control for reusable launch vehicle. Feasibility and validity of the new controller is demonstrated with simulation examples.
Keywords :
aircraft control; attitude control; control system synthesis; nonlinear control systems; observers; robust control; variable structure systems; control effect; controller stability; nonlinear dynamic inversion technique; nonlinear extended state observer; reentry attitude control; reusable launch vehicle; robust controller; self-regulation control scheme; sliding mode control; system disturbance; Conferences;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Advanced Computational Intelligence (ICACI), 2012 IEEE Fifth International Conference on
Conference_Location :
Nanjing
Print_ISBN :
978-1-4673-1743-6
Type :
conf
DOI :
10.1109/ICACI.2012.6463203
Filename :
6463203
Link To Document :
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