TY - GEN
T1 - Backstepping Sliding Mode Control for Missile Attitude System
AU - Zi-Rui, Huang
AU - Yun-Jie, Wu
AU - Jing-Xing, Zuo
AU - Ling, Cheng
N1 - Publisher Copyright:
© 2018 IEEE.
PY - 2018/8
Y1 - 2018/8
N2 - This paper is devoted to the attitude control of a quaternion described missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. One backstepping sliding mode controller is designed to guarantee the state variables of the closed-loop system to converge to a small region of the reference states. The variable structure control including sliding mode control has the valuable features of anti-interference and resisting parameter distortion, providing a useful solution for designing control law. Also, simulation results are presented to illustrate the effectiveness of the control strategy.
AB - This paper is devoted to the attitude control of a quaternion described missile model, which is nonlinear in aerodynamics with atmospheric moment uncertainties, inertia uncertainties, bounded disturbances and actuator failures. One backstepping sliding mode controller is designed to guarantee the state variables of the closed-loop system to converge to a small region of the reference states. The variable structure control including sliding mode control has the valuable features of anti-interference and resisting parameter distortion, providing a useful solution for designing control law. Also, simulation results are presented to illustrate the effectiveness of the control strategy.
KW - backstepping
KW - missile attitude control
KW - sliding mode control
UR - https://www.scopus.com/pages/publications/85082475995
U2 - 10.1109/GNCC42960.2018.9019024
DO - 10.1109/GNCC42960.2018.9019024
M3 - 会议稿件
AN - SCOPUS:85082475995
T3 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
BT - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
PB - Institute of Electrical and Electronics Engineers Inc.
T2 - 2018 IEEE CSAA Guidance, Navigation and Control Conference, CGNCC 2018
Y2 - 10 August 2018 through 12 August 2018
ER -