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