DocumentCode
1613027
Title
Optimal predictive controller design for reentry vehicle
Author
Peng Wang ; Guojian Tang ; Jie Wu
Author_Institution
Coll. of Aerosp. Sci. & Eng., Nat. Univ. of Defense Technol., Changsha, China
fYear
2013
Firstpage
322
Lastpage
326
Abstract
A Six Degrees of Freedom (Six-DoF) reentry vehicle model is being developed for control studies. This vehicle model is highly nonlinear, multivariable, unstable and coupling and includes uncertain parameters. An optimal predictive controller is designed according to the feature that reentry vehicle (RV) model is highly nonlinear, fast-variability, coupling, and with parameters of great uncertainties. This method contains two parts, which are inner-loop nonlinear generable predictive control (NGPC) system and outer-loop NGPC system, respectively. Simulation studies demonstrate that the proposed control method is feasible for RV. Simulation studies are conducted for initial conditions of altitude of 40km and velocity 4500m/s for the responses of the commands of angle of attack, sideslip angle and bank angle. The simulation studies demonstrate that the proposed controller is robust with respect to the interference and parametric uncertainties, and meets the performance requirements with acceptable control inputs.
Keywords
control system synthesis; nonlinear control systems; optimal control; predictive control; robust control; space vehicles; RV model; angle-of-attack command; bank angle command; degrees-of-freedom; inner-loop NGPC system; interference; nonlinear generable predictive control; optimal predictive controller design; outer-loop NGPC system; parametric uncertainties; robust control; sideslip angle command; six-DoF reentry vehicle model; Attitude control; Nonlinear systems; Predictive control; Predictive models; Robustness; Vectors; Vehicles; hierarchy-structured; optimal predictive control; reentry vehicle; robustness;
fLanguage
English
Publisher
ieee
Conference_Titel
Chinese Automation Congress (CAC), 2013
Conference_Location
Changsha
Print_ISBN
978-1-4799-0332-0
Type
conf
DOI
10.1109/CAC.2013.6775751
Filename
6775751
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