TY - JOUR
T1 - Design of a novel sliding mode controller for the attitude control of reentry vehicle
AU - Li, Xian Qiang
AU - Zhou, Jun
AU - Guo, Jian Guo
N1 - Publisher Copyright:
©, 2015, Journal of Solid Rocket Technology. All right reserved.
PY - 2015/6/1
Y1 - 2015/6/1
N2 - A novel sliding mode control method was proposed in this paper, which is not only capable of improving the robustness of the existing control law, but can also effectively attenuate chattering. In the design process, a novel dynamic sliding mode surface was designed firstly based on the nominal system and the existing control law. Then the super-twisted algorithm was improved. A fast continuous and finite time convergence algorithm was obtained, which was adopted as the novel reaching law for the first time. The reaching law combined with the sliding mode surface can greatly enhance the robustness of the existing control law. In addition, since the sliding mode switching law is continuous, the chattering was greatly attenuated. The proposed method was then applied to attitude tracking control of reentry vehicle and the robustness of the existing control law was effectively enhanced under large disturbance. Finally, the effectiveness of the method was demonstrated through simulation.
AB - A novel sliding mode control method was proposed in this paper, which is not only capable of improving the robustness of the existing control law, but can also effectively attenuate chattering. In the design process, a novel dynamic sliding mode surface was designed firstly based on the nominal system and the existing control law. Then the super-twisted algorithm was improved. A fast continuous and finite time convergence algorithm was obtained, which was adopted as the novel reaching law for the first time. The reaching law combined with the sliding mode surface can greatly enhance the robustness of the existing control law. In addition, since the sliding mode switching law is continuous, the chattering was greatly attenuated. The proposed method was then applied to attitude tracking control of reentry vehicle and the robustness of the existing control law was effectively enhanced under large disturbance. Finally, the effectiveness of the method was demonstrated through simulation.
KW - Chattering attenuate
KW - Dynamic sliding surface
KW - Reentry vehicle
KW - Siding mode control
KW - Super-twisting algorithm
UR - http://www.scopus.com/inward/record.url?scp=84937420906&partnerID=8YFLogxK
U2 - 10.7673/j.issn.1006-2793.2015.03.001
DO - 10.7673/j.issn.1006-2793.2015.03.001
M3 - 文章
AN - SCOPUS:84937420906
SN - 1006-2793
VL - 38
SP - 301
EP - 307
JO - Guti Huojian Jishu/Journal of Solid Rocket Technology
JF - Guti Huojian Jishu/Journal of Solid Rocket Technology
IS - 3
ER -