DocumentCode :
2098497
Title :
Blended control with lateral thrust and aerodynamic force based on predictive control
Author :
Yang Baoqing ; Bi Yongtao ; Yao Yu ; Jin Jing
Author_Institution :
Sch. of Astronaut., Harbin Inst. of Technol., Harbin, China
fYear :
2010
fDate :
29-31 July 2010
Firstpage :
6161
Lastpage :
6166
Abstract :
The blended control method of atmospheric missile with lateral thrust and aerodynamic force is investigated. Firstly, considering configuration of lateral jets, the model of blended control system is established. Secondly, the blended control strategy is proposed, this strategy consists of three components, i.e. dynamic distribution algorithm, direct force control subsystem, aerodynamic control subsystem. Considering the dynamic difference between the direct force control and aerodynamic control subsystem, the dynamic distribution algorithm of an over load error is given based on predictive control. Then, the direct force control law and aerodynamic control law are designed based on predictive control and ADRC. Lastly, the simulation results validate the effectiveness of the proposed method.
Keywords :
aerodynamics; attitude control; control system synthesis; force control; jets; missile control; predictive control; aerodynamic control law; aerodynamic force; atmospheric missile; blended control method; direct force control; lateral thrust; predictive control; Aerodynamics; Force; Force control; Heuristic algorithms; Missiles; Predictive control; ADRC; Blended Control; Dynamic Distribution; Lateral Thrust; Predictive Control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Control Conference (CCC), 2010 29th Chinese
Conference_Location :
Beijing
Print_ISBN :
978-1-4244-6263-6
Type :
conf
Filename :
5573097
Link To Document :
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